A

  • Abarghooei, Arash Attitude Control of Nanosatellite Using Optimal Quadratic Linear and Nonlinear Methods [Volume 16, English Special Issue, 2023, Pages 51-64]

  • Abbasi, Hossein Reza Design and Manufacture of Thermal Model of AUTSAT Satellite and Its Thermal Balance Test [Volume 9, Issue 2, 2016, Pages 61-76]

  • Abbasi, Yosof Re-Entry Trajectory Design with Use of Aided Optimization Algorithm through Combination of Classic Guidance & Acceleration Profile Optimization [Volume 15, Issue 1, 2022, Pages 51-62]

  • Abbasi-Moghadam, D Electro-Optical Design of Imaging Payload for a Remote Sensing Satellite [Volume 2, Issue 3, 2009, Pages 57-70]

  • Abbasi-Moghadam, D. هدایت بهینه بر خط بازگشت به زمین از طریق بسط مجانبی هماهنگ [Volume 3, Issue 2, 2011, Pages 69-76]

  • Abdi, Gh. Automatic Navigation of Aerial Vehicles on a Vision-Aided Navigation System [Volume 5, Issue 1, 2012, Pages 1-14]

  • Abdolahi, Sohayla Aerodynamic Heating Prediction of Flying Body Using Fluid-Solid Conjugate Heat Transfer [Volume 8, Issue 3, 2015, Pages 41-53]

  • Abdollahi, T. Effects of Solar Activities, Drag Coefficient and Atmospheric Wind on Altitude Loss of a LEO Satellite [Volume 1, Issue 1, 2008, Pages 57-66]

  • Abdollahi Azgomi, Mohammad Software Fault Tolerance Techniques for Dealing with Transient Faults in Satelite Software [Volume 5, Issue 4, 2013, Pages 9-18]

  • Abdoullah-Mianji, F. Design and Simulation of Magnetic Conductors to Enhance Features of Satellite Antennas and to Reduce Effects of Space Radiation [Volume 6, Issue 3, 2013, Pages 61-66]

  • Abedi, M. Design of Fault Detection, Identification and Recovery Algorithms for a 3-Axis Stabilized Satellite [Volume 5, Issue 1, 2012, Pages 29-40]

  • Abedi, M. Design of Fault Detection, Isolation and Accommodation Algorithm for Attitude Determination System of a 3-Axis Satellite [Volume 5, Issue 2, 2012, Pages 1-13]

  • Abedi, M. Design of Adaptive Threshold Based Fault Detection and Isolation for Attitude Control System of a Three Axis Satellite [Volume 6, Issue 1, 2013, Pages 31-46]

  • Abedi, Mohsen Modeling and calculating the albedo and IR heat flux applied to satellite based on the geographic position of sarellite [Volume 11, Issue 4, 2018, Pages 23-30]

  • Abedi, Mohsen Multi objective design optimization of heat pipes configuration attached to the solar panels of a sun pointing satellite [Volume 12, Issue 1, 2019, Pages 55-68]

  • Abedian, A. Designing, Testing and Evaluation of Single Gimbal Control Moment Gyro for Microsatellite [Volume 2, Issue 1, 2009, Pages 13-23]

  • Adami, A. H. Introducing of Attitude Determination System of a LEO Satellite with Orbital Maneuver Mission [Volume 4, Issue 2, 2012, Pages 1-10]

  • Adami, AmirHoseyn Specific Grain Analysis and Rapid Internal Ballistic Simulation for Solid Motor [Volume 5, Issue 3, 2012, Pages 67-80]

  • Adami, Amirhossain Monopropellant Propulsion System Design using Multidisciplinary Design Optimization, Sequential Design Method, and Comparing Results [Volume 10, Issue 2, 2017, Pages 53-63]

  • Adami, Amirhossain Robust Guidance Algorithmfor Reentry Vehicles based on PLS Regression in the Presence ofInitail Parameter Uncertainties [Volume 10, Issue 4, 2018, Pages 29-40]

  • Adami, Amirhossain Nonlinear Optimal Control of Reentry Vehicles Based on Deriving the State and Control Depended Systematic Matrices in State Space Form [Volume 11, Issue 1, 2018, Pages 1-12]

  • Adami, Amirhossain Introducing and implementation of nested dependency method to estimate the behavior of spatial structures of a Reentry Capsule [Volume 11, Issue 4, 2018, Pages 43-50]

  • Adami, Amirhossain Evaluation of Three Design approach of a bipropellant propulsion system including multidisciplinary design optimization, Robust and Optimum-Robust [Volume 12, Issue 1, 2019, Pages 41-53]

  • Adami, Amirhossain Design of an Upper Stage Propulsion System by Multi Objective Hybrid PSO [Volume 13, Issue 3, 2020, Pages 1-16]

  • Adami, Amirhossain The presentation of the ARTA CanSat design and construction process at the CANSAT International Competition in Iran [Volume 13, Issue 2, 2020, Pages 63-77]

  • Adami, Amirhossain Performance evaluation of a launch vehicle with non-turbopump propulsion system based on multidisciplinary analysis (MDA) [Volume 14, Issue 4, 2021, Pages 35-49]

  • Adami, Amirhossain Multidisciplinary Design of Bipropellant Propulsion System in Three Methods, Optimal Design, Reliability Based Design and Optimal Reliability Based Design [Volume 14, Issue 4, 2021, Pages 85-98]

  • Adami, Amirhossain Multi-Disciplinary Optimization Conceptual Design of the Launcher Based on Non-Turbopump Propulsion Systems [Volume 15, Issue 1, 2022, Pages 121-137]

  • Adami, Amirhossain Introducing the Nonlinear State Control Algorithm of the Air Bearing Laboratory Simulator Based on the Gain Coefficients Dependent on the State Variables [Volume 16, Issue 3, 2023, Pages 79-89]

  • Adami, Amirhossain Introducing the conceptual design process of the Armita lunar rover Based on ECSS [(Articles in Press)]

  • Adami-Dehkordi, A. h. Multidisciplinary Conceptual Design Optimization of Monopropellant Propulsion System of Nanosatellite [Volume 3, Issue 2, 2011, Pages 11-22]

  • Adami-Dehkordi, A. H. An Algorithm for Increasing Performance of a Space Launch Vehicle Using Solid Rocket Boosters [Volume 2, Issue 1, 2009, Pages 67-71]

  • Afsari, Narges The presentation of the ARTA CanSat design and construction process at the CANSAT International Competition in Iran [Volume 13, Issue 2, 2020, Pages 63-77]

  • Afshari, Ebrahim Effects of Geometrical Parameters of Gas Flow Channels on Polymer Electrolyte Membrane Fuel Cell Performance [Volume 15, English Special Issue, 2022, Pages 1-13]

  • Aghaei, A. Design and Fabrication of Laboratory Pilot for OSL Dosimeter System for Space Applications [Volume 6, Issue 3, 2013, Pages 67-73]

  • Aghaei, M.B Measurement of Neutron Irradiation Effect on Reverse Current Damage Constant α for Diode [Volume 6, Issue 2, 2013, Pages 11-19]

  • Aghaei, Morteza High Efficiency Converter for Satellite Power Amplifier Stage [Volume 11, Issue 1, 2018, Pages 41-48]

  • Aghajani, Zeynab GEO Communication Satellite Engineering Design Code [Volume 10, Issue 4, 2018, Pages 41-54]

  • Aghalari, Alireza Attitude Stability Testing of an Agile Satellite Simulator with Single-Gimbal Control-Momentum-Gyros [Volume 5, Issue 4, 2013, Pages 61-68]

  • Aghalari, Alireza Designing and Implemntation of PID and Feed back Quaternion Control Strategies for Three Axis Satellite Simulator Equipped With Control Moment Gyros Actiatprs [Volume 9, Issue 1, 2016, Pages 13-23]

  • Aghalari, Ali Reza Design and Manufacturing of a Variable Speed Control Moment Gyro for an Agile Micro-Satellite Attitude Control Simulator [Volume 8, Issue 1, 2015, Pages 73-77]

  • Aghalari, A. R. Designing, Testing and Evaluation of Single Gimbal Control Moment Gyro for Microsatellite [Volume 2, Issue 1, 2009, Pages 13-23]

  • Aghalari, A. R. Development of Reaction Wheel Disturbances General Model and Validation with Experimental Data [Volume 6, Issue 1, 2013, Pages 79-91]

  • Aghalari, A.R. Design, Manufacturing and Test of a Three Degrees-of-Freedom Attitude Control Simulator for an Agile Micro-Satellite Based on Single Gimbal Control Moment Gyros [Volume 7, Issue 3, 2014, Pages 51-67]

  • Aghamohammadi, Hossein Developing web-based geographical services for temporally vegetation status monitoring using satellite imagery [Volume 13, Issue 4, 2020, Pages 49-58]

  • Ahangar, M. An Investigation on the Effect of Chemical Kinetics Mechanisms in the Modeling of Combustive Gaseous Oxidizer Flow on a Solid Fuel Surface [Volume 3, Issue 1, 2010, Pages 1-13]

  • Ahangar, Mahdy Numerical Modeling of plasma flow in an Electrohydrodynamic thruster with two-cathode electrode arrangement [Volume 12, Issue 2, 2019, Pages 1-10]

  • Ahangarani Farahani, Alireza A New Adaptive Controller for the Three ‎Axis Satellite Simulator Based on Continuous ‎Time Delay Petri Nets Tool [Volume 16, English Special Issue, 2023, Pages 25-38]

  • Ahangarani Farahani, Alireza Introducing the Nonlinear State Control Algorithm of the Air Bearing Laboratory Simulator Based on the Gain Coefficients Dependent on the State Variables [Volume 16, Issue 3, 2023, Pages 79-89]

  • Ahangarani Farahani, Alireza Introducing the conceptual design process of the Armita lunar rover Based on ECSS [(Articles in Press)]

  • Ahmadi, Alireza Rapid Performance Sizing of Reaction Wheels in a Very High Resolution Remote Sensing Satellite Using Matching Diagram Technique [Volume 15, Issue 1, 2022, Pages 21-39]

  • Ahmadi, Amir Hossin Investigating the Test and Evaluation of GaN Transistors Radiation Resistance in SSPA Amplifier Board in LEO Satellite Payload [Volume 16, Issue 1, 2023, Pages 59-74]

  • Ahmadloo, A. Considerations of Utilizing Telemetry and GPS System in Sounding Rockets [Volume 1, Issue 1, 2008, Pages 81-86]

  • Ajami, Atefe Design a Model of Four Color Separation Prism in Satellite Camera [Volume 5, Issue 3, 2012, Pages 41-48]

  • Ajorkar, Abbas Design and Implementation of Backstepping-Sliding mode Attitude Controller in The Prossecor in The Loop Test Bed [Volume 9, Issue 1, 2016, Pages 25-35]

  • Akbari, Bhzad Comparison of Direct and Indirect Georeferencing Methods Using Satellite Linear Array Iimages [Volume 8, Issue 2, 2015, Pages 1-10]

  • Akhlaghi, A. M. Reliability Allocation to Launch Vehicle Subsystems by Using AHP Method in Conceptual Design Phase [Volume 5, Issue 2, 2012, Pages 49-57]

  • Akhlomadi, M. R Nonlinear Optimal Control of Space Docking and Rendezvous Problem [Volume 8, Issue 3, 2015, Pages 27-40]

  • Alavi, E. The Study of Hypergravity and Flight Stress on Different Cell Lines Function in Sounding Rocket [Volume 6, Issue 4, 2014, Pages 37-42]

  • Alavi pour, Mojtaba Optimal Trajectory Design of an Upper Stage for Satellite Injection into Geostationary Orbit Using Limited Thrust [Volume 9, Issue 4, 2017, Pages 13-25]

  • Alemi Naeeni, A. R. Developing a New Explicit Guidance Method for the Trajectory Correction of Sub-Orbital Modules [Volume 6, Issue 3, 2013, Pages 15-26]

  • Alemi Naeeni, A. R. Developing a Multi-Objective Guidance Scenario for the Entry to the Earth’s Atmosphere [Volume 6, Issue 4, 2014, Pages 53-62]

  • Alemi Rostami, Mehdi Evaluation of Diversity Effects on Increasing the Reliability of Space Systems [Volume 15, English Special Issue, 2022, Pages 45-53]

  • Alemi Rostami, Mehdi Increasing the Efficiency and Reliability of the High-Power Supply With the Application of TWTA Lamps [Volume 17, Issue 1, 2024, Pages 37-48]

  • Alidoust, L. The Study of Hypergravity and Flight Stress on Different Cell Lines Function in Sounding Rocket [Volume 6, Issue 4, 2014, Pages 37-42]

  • Alikhani, Alireza Thermal Optimum Trajectory Design of Manned Reentry Vehicles using the Aerodynamic Database Management Method [Volume 13, Issue 2, 2020, Pages 51-61]

  • Alikhani, Ali Reza Optimal Control of a Flexible Spacecraft in a Proximity Operation Using State Dependent Riccati Equation Approach [Volume 8, Issue 1, 2015, Pages 27-41]

  • Alikhani, Ali Reza Guidance and Control for Space Capsule in the Presence of Uncertain Dynamic Parameters during the Atmospheric Entry Phase [Volume 8, Issue 3, 2015, Pages 1-13]

  • Alikhani, Ali Reza Dynamic Terminal Sliding Mode Control for an Aerospace Launch Vehicle [Volume 8, Issue 4, 2016, Pages 1-7]

  • Alikhani, َAlireza Design, Construction and Performance Evaluation of a Cold Gas Thruster Test Stand [Volume 15, English Special Issue, 2022, Pages 55-64]

  • Alikhani, َAlireza Attitude and Vibration Control of a Flexible Spacecraft Using Hybrid Adaptive Super-Twisting Non-Singular Terminal Sliding Mode Control [Volume 16, Issue 4, 2023, Pages 1-13]

  • Alikhani, Mohammda Reza Dynamic & Non-linear Modelling of an Expansion Cycle Rocket Engine [Volume 13, Issue 1, 2020, Pages 39-48]

  • Ali Mohammadi, H. R. Using Response Surface Method (RSM) in the Optimal Allocation of Tolerances [Volume 4, Issue 1, 2011, Pages 61-67]

  • Ali Mohammadi, H. R. Dynamics Simulation of Pressurizing in Propulsion System Configuration [Volume 6, Issue 3, 2013, Pages 1-13]

  • Alimohammadi Sarab, Abbas Improvement of Forest Canopy Density Model Using Remote Sensing Data Integration [Volume 12, Issue 3, 2019, Pages 31-42]

  • Ali Mohammady, H. R. Study of Hot Gas Pressurizing System Tank and Liquid Rocket Engine Interaction by Dynamic Simulation [Volume 6, Issue 1, 2013, Pages 11-19]

  • Aliparast, Peiman Design of an Electromagnetic Band Gap Shield for a Ku-Band VSAT Transmitter Power Amplifier [Volume 14, Issue 1, 2021, Pages 35-41]

  • Aliparast, Peyman design, implementation and test of acoustic data acquisition subsystem for space Bio-capsule of Pajohesh explorer [Volume 13, Issue 3, 2020, Pages 17-24]

  • Alipoor, Ali System Design and Simulation of Air-Spacecraft Aerospike Nozzle by Utilizing the Computational Fluid Dynamics (CFD) Method [Volume 16, Issue 1, 2023, Pages 23-34]

  • Alirezapouri, Mohammad Ali Usinge The qEKF Algorithm for Satellite Attitude Estimation with Two Magnetometer & Sun Sensors [Volume 14, Issue 3, 2021, Pages 65-73]

  • Alisadeghi, Hamed Evaluation of Effective Emissivity of a Multilayer Insulation Blanket Using Test [Volume 8, Issue 1, 2015, Pages 19-25]

  • Alisadeghi, Hamed Dimensional Direct Simulation Monte Carlo Simulation of Thruster Plumes [Volume 15, Issue 2, 2022, Pages 43-58]

  • Alisadesghi, hamed Design and Manufacture of Thermal Model of AUTSAT Satellite and Its Thermal Balance Test [Volume 9, Issue 2, 2016, Pages 61-76]

  • Aliyari, M. Fault Detection for an Aerospace Launch Vehicle Using Sliding Mode Observer [Volume 6, Issue 2, 2013, Pages 49-56]

  • Alizadeh, Behzad Magnetic field effects on heat transfer enhancement in an enclosure in microgravity conditions [Volume 13, Issue 4, 2020, Pages 59-69]

  • AlizadehYazdi, Mehdi Experimental Analysis of Pyroshock Wave Propagation in Kavoshgar's Payload [Volume 7, Issue 4, 2015, Pages 51-62]

  • Allagheband Hosseini, Y. An Analysis of the Possiblity of Applying the Provisions of the Rescue and Return Agreement to Space Tourists [Volume 6, Issue 1, 2013, Pages 21-30]

  • Allahverdizadeh, Firouz Design of an Nonlinear Extended State Observer to Estimate Unmeasurable Information on the Problem of Flying Objects Guidance [Volume 15, Issue 3, 2022, Pages 67-78]

  • Amani, E. کاربرد مدل پاندول ساده به منظور اعمال دینامیک تلاطم سیال در شبیه‌سازی شش درجه آزادی پرواز ماهواره‌بر [Volume 3, Issue 2, 2011, Pages 59-67]

  • Amin, S. Designing and Constructing of Inverted F Antennas on a Space Bound Vehicle for Telemetry Transmission [Volume 1, Issue 2, 2008, Pages 57-60]

  • Aminzadeh, Ali Vibration Control Design of Fuel Sloshing in a Spacecraft Using Virtual Actuator [Volume 15, Issue 1, 2022, Pages 63-71]

  • Aminzadeh, E. An Analysis of the Possiblity of Applying the Provisions of the Rescue and Return Agreement to Space Tourists [Volume 6, Issue 1, 2013, Pages 21-30]

  • Amiri, Ebrahim Economic analysis of exploitation of lunar resources [(Articles in Press)]

  • Amiri, Sh. GPS Radio Occultation Method for Ionosphere TEC Monitoring [Volume 6, Issue 2, 2013, Pages 21-28]

  • Amiri, Shervin GPS Signal Simulation in Intermediate Frequency (IF) [Volume 5, Issue 3, 2012, Pages 33-40]

  • Amiri, Shervin Atmospheric Doppler Modelling for Open Loop Tracking in GPS-RO Receivers [Volume 9, Issue 2, 2016, Pages 35-46]

  • Amiri Atashgah, MohammadAli Orbit Determination via a Deeply- Coupled UKF/GNSS Filter [Volume 9, Issue 3, 2016, Pages 13-26]

  • Amiri Atashgah, MohammadAli Localization of Aerial Robot Based on Fisheye Cameras in a Virtual Lab [Volume 14, Issue 2, 2021, Pages 49-59]

  • Amirifar, Mohammadali Effect of Injector Pressure Drop on The ‎Performance of A 1 N Monopropellant ‎Thruster [Volume 15, Issue 4, 2022, Pages 19-29]

  • Amirifar, Mohammad Ali Investigation on Performance Characteristics of Hydrazine Monopropellant Thruster according to Reaction Chamber Adiabatic Temperature [Volume 15, Issue 3, 2022, Pages 33-47]

  • Amiri -Simkooei, Ali Reza GPS-RTK Integrated with Micro-Electro Mechanical INS for Precise Application [Volume 5, Issue 3, 2012, Pages 49-57]

  • Amjadifard, R. Evaluation of the Effects of Radiation, Irradiance, and Temperature on Solar Cell Electrical Characteristics and Extraction of Maximum Solar Panel Power by MPPT [Volume 1, Issue 1, 2008, Pages 67-80]

  • Amjadifard, Reza System-level Evaluation of the Operation of Different Solar Array Structures for Various CubeSat Configurations [Volume 15, Issue 3, 2022, Pages 93-108]

  • Amjadifard, Reza Studying the Effects of Multi-Layer Shielding in Reducing Space Radiations Exposure of Human and Electrical Components in Space Missions [Volume 16, Issue 2, 2023, Pages 19-26]

  • Amjadifard, Reza Identification and Prioritization of Satellite Electrical Power Subsystem Technologies for National Development Based on Multiple Criteria Decision Making [(Articles in Press)]

  • Anbarloi, M. Design and Manufacturing a Laboratory Example of Pulsed Plasma Thruster [Volume 3, Issue 2, 2011, Pages 23-30]

  • Anvari, A. Determination of Deployment Angle for the Optimum Operation of Solar Panels Used in a LEO Satellite [Volume 1, Issue 2, 2008, Pages 1-8]

  • Anvari, A. Effects of Some Parameters on Thermal Control of a LEO Satellite [Volume 7, Issue 1, 2014, Pages 13-24]

  • Arabian, M. The Study of Hypergravity and Flight Stress on Different Cell Lines Function in Sounding Rocket [Volume 6, Issue 4, 2014, Pages 37-42]

  • Arabian Arani, Ali Proportional Navigation Guidance with Variable Navigation Ratio in terms of the angle of relative velocity with respect to Line-of-Sight and its Rate [Volume 13, Issue 2, 2020, Pages 1-12]

  • Arabian Arani, Ali Proportional Navigation with Linear Acceleration and Line-of-Sight Acceleration Feedbacks [Volume 13, Issue 4, 2020, Pages 1-13]

  • Arabian Arani, Ali Miss Distance Analysis of First-Order Explicit Guidance Law with/without Radome effect [Volume 15, Issue 4, 2022, Pages 1-18]

  • Arabshahi, Hamid Online Optimal Integrated Guidance and Control Algorithm Design for Launch Vehicle [Volume 8, Issue 2, 2015, Pages 67-78]

  • Arabsorkhi, Mahboube Design a Model of Four Color Separation Prism in Satellite Camera [Volume 5, Issue 3, 2012, Pages 41-48]

  • Aramkhah, Kosar Symmetric periodic solution around asteroid 216 Kleopatra and its stability in the presence of solar radiation pressure [Volume 14, Issue 1, 2021, Pages 1-13]

  • Arbabmir, Mohammadvali A Survey on Vision Navigation Methods for UAV Navigation Applications [Volume 10, Issue 2, 2017, Pages 33-52]

  • Arbabmir, Mohammadvali Visual-Inertial Navigation System based on a New approach in Tracking and Investigating the Image Feature Points [Volume 12, Issue 3, 2019, Pages 43-54]

  • Arefkhani, Hamed Satellite Spin Stabilization by Magnetic Torquers and Validation with Air-Bearing Simulator [Volume 9, Issue 2, 2016, Pages 25-34]

  • Arefkhani, Hamed Evaluation of Magnetic Attitude control with Air-Bearing simulator [Volume 9, Issue 2, 2016, Pages 47-60]

  • Arefkhani, Hamed Introducing the Nonlinear State Control Algorithm of the Air Bearing Laboratory Simulator Based on the Gain Coefficients Dependent on the State Variables [Volume 16, Issue 3, 2023, Pages 79-89]

  • Ariaeifar, N. Analysis of Random Positioning System for Simulation of Microgravity [Volume 2, Issue 1, 2009, Pages 25-34]

  • Ariaii-Far, N. Investigation and Analysis of Seperation System of Kavoshgar-3 [Volume 3, Issue 1, 2010, Pages 15-23]

  • Arvan, Mohammad Reza Integrated Guidance and Control Design by Combining Backstepping and Sliding Mode Control Methods [Volume 9, Issue 4, 2017, Pages 39-50]

  • Aryanian, Iman Experimental Study of the Effect of Using Space Sandwich Structures for Protection Against Space Radiation [Volume 15, Issue 2, 2022, Pages 59-69]

  • Asadian, Nima Development of an Integrated Design Environment for Optimal Ascent Trajectory Planning [Volume 1, Issue 1, 2008, Pages 1-10]

  • Asadi golzar, Mohammad The Effects of Simulated Microgravity on Serum Levels of VEGF in Male Wistar Rats [Volume 9, Issue 4, 2017, Pages 63-68]

  • Asdaghpour, Fatemeh Thermal Effects of the Space Environment on the Radiation Characteristics of a Reflector Antenna in LEO Satellite [Volume 15, Issue 2, 2022, Pages 103-113]

  • Asgari, Jamal GPS-RTK Integrated with Micro-Electro Mechanical INS for Precise Application [Volume 5, Issue 3, 2012, Pages 49-57]

  • Asghari, Isa Design, Manufacture and Experimental Study of a Hydrogen Peroxide-HTPB Hybrid Rocket Motor [Volume 5, Issue 4, 2013, Pages 19-28]

  • Asghari, M. Dynamic Simulation for Diffusion of Satellite Detached Particles in Various Orbits [Volume 2, Issue 1, 2009, Pages 59-65]

  • Ashjaee, Mehdi Numerical Simulation and Optimization of Forced Convection Heat Transfer of Magnetic Nanofluid in a Channel in the Presence of a Non-Uniform Magnetic Field [Volume 11, Issue 2, 2018, Pages 11-19]

  • Ashtari, M. H. Analysis of Navid Satellite TLE Data and it’s Effects on Tracking Operations by the Ground Stations [Volume 6, Issue 2, 2013, Pages 29-42]

  • Ashtari, M. H. Increasing Accuracy of Satellite Position Prediction with Considering Harmonics of Potential Function of the Earth [Volume 6, Issue 3, 2013, Pages 27-37]

  • Ashtari, Mohammad Hassan Introduction to Tadbir satellite Orbit Determination System [Volume 8, Issue 3, 2015, Pages 65-70]

  • Askari Mahdavi, S. Atomyzasion Modeling the Rotating Spray Slime [Volume 4, Issue 1, 2011, Pages 39-48]

  • Aslani, Gholamreza Calculation and measurement of leakage current variations due to displacement damage for a silicon diode exposed to space protons [Volume 13, Issue 4, 2020, Pages 71-79]

  • Azadi, Emad Active Control of a Smart Satellite under Thermal Loading [Volume 8, Issue 1, 2015, Pages 43-51]

  • Azadi, Mohammad Active Control of a Smart Satellite under Thermal Loading [Volume 8, Issue 1, 2015, Pages 43-51]

  • Azadnejad, Saeed Improvement of the forest canopy density model based on the addition of the FCC index and the average kernel implementation [Volume 14, Issue 2, 2021, Pages 27-36]

  • Azimi, Asghar Design, Fabrication, and Test of a Cryogenic Liquid Oxygen-Ethanol Engine [Volume 16, Issue 1, 2023, Pages 47-58]

  • Azodi, Armin Parametric Study of Aeroelastic Instability Boundaries of Space Launch Vehicle in Subsonic Flow [Volume 15, Issue 3, 2022, Pages 49-66]

B

  • Babaei, Hamed Design, Simulation, Fabrication and Determining the Equivalent Circuit Model of a Reconfigurable FSS unit Cell Filter for Electromagnetic Protection of Space Payload Systems [Volume 16, Issue 4, 2023, Pages 71-82]

  • Bagheri, A. Modeling and Evaluation of Reliability in Rocket Engine by Fault Tree Analysis [Volume 2, Issue 2, 2009, Pages 69-73]

  • Bagherian, M Flight Path Angle Steering with Lambert Guidance Reference [Volume 2, Issue 2, 2009, Pages 75-79]

  • Bagheroskouei, Farhad System-level Evaluation of the Operation of Different Solar Array Structures for Various CubeSat Configurations [Volume 15, Issue 3, 2022, Pages 93-108]

  • Bagheroskuee, Farhad Identification and Prioritization of Satellite Electrical Power Subsystem Technologies for National Development Based on Multiple Criteria Decision Making [(Articles in Press)]

  • Bahmani nejad, Morteza Experimental Study of the Effect of Using Space Sandwich Structures for Protection Against Space Radiation [Volume 15, Issue 2, 2022, Pages 59-69]

  • Bahrami, M. Considerations of Utilizing Telemetry and GPS System in Sounding Rockets [Volume 1, Issue 1, 2008, Pages 81-86]

  • Bahrami, M. Designing and Constructing of Inverted F Antennas on a Space Bound Vehicle for Telemetry Transmission [Volume 1, Issue 2, 2008, Pages 57-60]

  • Bahrami, M. Investigation and Analysis of Seperation System of Kavoshgar-3 [Volume 3, Issue 1, 2010, Pages 15-23]

  • Bahrami, M. Required Velocity Calculation in the Presence Of Atmosphere Effect in C* Matrix [Volume 4, Issue 1, 2011, Pages 69-78]

  • Bahrami, M. Robust Control of Spacecraft Formation Flying Using Optimal Sliding Mode [Volume 6, Issue 1, 2013, Pages 69-75]

  • Bahrami, M. The Study of Hypergravity and Flight Stress on Different Cell Lines Function in Sounding Rocket [Volume 6, Issue 4, 2014, Pages 37-42]

  • Bahrami, M. Fuzzy Sliding Mode for Spacecraft Formation Control in Eccentric Orbits [Volume 7, Issue 1, 2014, Pages 49-56]

  • Bahrami, Mohsen Verification of a Low Cost Method for Accelerometers Calibration with a Two-Axis Table [Volume 7, Issue 4, 2015, Pages 73-79]

  • Baradaran Shokouhi, Sh. Satellite Camera CCD Read-out System Design, Based on Noise Optimization with Respect to Satellite Limitations [Volume 2, Issue 3, 2009, Pages 19-26]

  • Baradaran Shokouhi, Sh. A Spin Satellite Imaging System Design with Real Time Imaging Capability Using FPGA [Volume 3, Issue 1, 2010, Pages 45-54]

  • Barati, Ghodratollah Introduction to Tadbir satellite Orbit Determination System [Volume 8, Issue 3, 2015, Pages 65-70]

  • Barati, M. Dynamics Modeling of Spacecraft Formation Flying and Evaluating the Models Accuracy under the Effects of Relative Distance, Eccentricity and Earth Gravitational Perturbation [Volume 5, Issue 1, 2012, Pages 51-59]

  • Barghi Zanjani, Hakime An Optimal Power Allocation in Multi-Beam Satellite Communication Systems Including Inter-Beam Interference by Particle Swarm Optimization (PSO) [Volume 10, Issue 1, 2017, Pages 55-60]

  • Barkhordar, A. Numerical Simulation of Complicated Grain Burnback in Three Dimensions [Volume 5, Issue 1, 2012, Pages 15-28]

  • Basohbat Novinzadeh, Ali Reza Integrated Design of Orbital Transfer Block in an Optimized and Multistep Converged Environment [Volume 7, Issue 4, 2015, Pages 23-37]

  • Basohbat Novinzadeh, Ali Reza Solid Fuel Orbiter Designe in Optimized Space Transfer [Volume 8, Issue 1, 2015, Pages 53-60]

  • Bataleblu, A. Survey on Nondeterministic Optimal Design and Its Applications in the Aerospace Industry [Volume 4, Issue 2, 2012, Pages 23-34]

  • Batrakoff, Vladimir A Method for Determining Design Parameters of Space Umbrella Antenna [Volume 15, Issue 4, 2022, Pages 31-43]

  • Bazrafshan, H. Satellite Camera CCD Read-out System Design, Based on Noise Optimization with Respect to Satellite Limitations [Volume 2, Issue 3, 2009, Pages 19-26]

  • Bazrafshan, H. A Spin Satellite Imaging System Design with Real Time Imaging Capability Using FPGA [Volume 3, Issue 1, 2010, Pages 45-54]

  • Bazrafshan, Jaafar A Reconfigurable and Steerable Horn Antenna Using Plasma Dielectric Slabs for Controllable Gain and Beam Steering [(Articles in Press)]

  • Bazregarzadeh, Elham New Approach in Guidance Law Design Based on Finite-Time Partial Stability Theorem [Volume 8, Issue 1, 2015, Pages 1-7]

  • Beheshti Boroumand, B. Considerations of Utilizing Telemetry and GPS System in Sounding Rockets [Volume 1, Issue 1, 2008, Pages 81-86]

  • Behnamgol, Vahid A New Backstepping Sliding Mode Guidance Law Considering Control Loop Dynamics [Volume 8, Issue 4, 2016, Pages 9-17]

  • Behnamgol, Vahid Finite Time Guidance Law to Intercept Desired LOS Angle Using NTSM Control [Volume 11, Issue 2, 2018, Pages 1-10]

  • Behnamgol, Vahid Lyapunov-basedAdaptive SmoothSecond-order Sliding Mode Guidance Law with Proving Finite Time Stability [Volume 11, Issue 2, 2018, Pages 33-39]

  • Behnam Gol, Vahid Design of an Nonlinear Extended State Observer to Estimate Unmeasurable Information on the Problem of Flying Objects Guidance [Volume 15, Issue 3, 2022, Pages 67-78]

  • Behzad Fallahpour, Mojtaba Design of a Multiband and Wide Angle Reflector [Volume 12, Issue 4, 2019, Pages 47-56]

  • Behzadi, Milad Numerical Investigation of Laminar Premixed Conical Flame Response to Acoustic Excitation [Volume 8, Issue 1, 2015, Pages 9-18]

  • Bemani, Vali Integrated Design of Orbital Transfer Block in an Optimized and Multistep Converged Environment [Volume 7, Issue 4, 2015, Pages 23-37]

  • Binazadeh, Tahere New Approach in Guidance Law Design Based on Finite-Time Partial Stability Theorem [Volume 8, Issue 1, 2015, Pages 1-7]

  • Binazadeh, Tahereh Velocity and Body Rate Control of a Spacecraft Using Robust Passivity-Based Control [Volume 11, Issue 2, 2018, Pages 41-46]

  • Blochestani, V. An Algorithm for Increasing Performance of a Space Launch Vehicle Using Solid Rocket Boosters [Volume 2, Issue 1, 2009, Pages 67-71]

  • Bod, Mohammad Gap Analysis in Satellite Communication Services [Volume 16, Issue 4, 2023, Pages 29-40]

  • Bohlouri, Vahid HIL Experimental Analyses of Satellite Electrical Power Subsystem (EPS) in De-tumbling Mode [Volume 10, Issue 4, 2018, Pages 19-28]

  • Bohlouri, Vahid Robust Optimization of Satellite Attitude Control with Thruster Actuators based on Combined Objective Function [Volume 10, Issue 4, 2018, Pages 55-66]

  • Bohlouri, Vahid Damping mode of satellite angular velocity using magnetic actuators in hardware/software in the loop [Volume 12, Issue 4, 2019, Pages 57-67]

  • Bohlouri, Vahid Study of Space Weather and its Risks on Human Biologic Processes [Volume 16, Issue 3, 2023, Pages 51-68]

  • Bohlouri, Vahid Design and implementation of hardware-in-the-loop (HIL) test-bed for spacecraft attitude control [Volume 12, Issue 2, 2019, Pages 55-70]

  • Bolandi, H. Design of Attitude Control System of an Axisymmetric Satellite with Gravity Gradient Stabilization and Slow Spinning about Yaw Axis [Volume 1, Issue 1, 2008, Pages 11-19]

  • Bolandi, H. Design of an Attitude Control System for a Stereo-Imagery Satellite with Combining of Along-Track and Across-Track Configurations [Volume 1, Issue 2, 2008, Pages 9-15]

  • Bolandi, H. Design of Attitude Control System of an Axisymmetric Satellite with Gravity Gradient Stabilization and Slow Spinning about Yaw Axis [Volume 1, Issue 2, 2008, Pages 27-33]

  • Bolandi, H. Design of an Attitude Estimation Algorithm for a LEO Satellite Based on Multiple Models Adaptive Method and Comparison with EKF [Volume 2, Issue 2, 2009, Pages 17-26]

  • Bolandi, H. Design of Fault Detection, Identification and Recovery Algorithms for a 3-Axis Stabilized Satellite [Volume 5, Issue 1, 2012, Pages 29-40]

  • Bolandi, H. Satellite Thermal Modeling and Analysis with the Electrical Network Method [Volume 5, Issue 1, 2012, Pages 81-90]

  • Bolandi, H. Design of Fault Detection, Isolation and Accommodation Algorithm for Attitude Determination System of a 3-Axis Satellite [Volume 5, Issue 2, 2012, Pages 1-13]

  • Bolandi, H. Design of Adaptive Threshold Based Fault Detection and Isolation for Attitude Control System of a Three Axis Satellite [Volume 6, Issue 1, 2013, Pages 31-46]

  • Bolandi, H. Analysis of Navid Satellite TLE Data and it’s Effects on Tracking Operations by the Ground Stations [Volume 6, Issue 2, 2013, Pages 29-42]

  • Bolandi, H. Increasing Accuracy of Satellite Position Prediction with Considering Harmonics of Potential Function of the Earth [Volume 6, Issue 3, 2013, Pages 27-37]

  • Bolandi, Hossean Introduction to Tadbir satellite Orbit Determination System [Volume 8, Issue 3, 2015, Pages 65-70]

  • Boorboor, S. Sensitive Volume Modeling in Calculation of Space Radiation-Induced SEU Cross Section [Volume 6, Issue 4, 2014, Pages 23-28]

  • Boostan, Danial Predicting Orbital State Vector of Satellites Using Time-Series Neural Networks [Volume 11, Issue 3, 2018, Pages 47-61]

  • Broomandnezhad, Tahereh Software Fault Tolerance Techniques for Dealing with Transient Faults in Satelite Software [Volume 5, Issue 4, 2013, Pages 9-18]

  • Bustan, D. Intelligent Satellite Orbit Prediction Based on Time Series Analysis [Volume 7, Issue 3, 2014, Pages 43-49]

  • Bustan, Daniyal Nonlinear Dynamic Inversion Fault Tolerant Control for Spacecraft    [Volume 8, Issue 2, 2015, Pages 11-17]

C

  • Cheheltani, S. H. Design, Manufacturing and Test of a Three Degrees-of-Freedom Attitude Control Simulator for an Agile Micro-Satellite Based on Single Gimbal Control Moment Gyros [Volume 7, Issue 3, 2014, Pages 51-67]

  • Chekini, A. FPGA Implementation of JPEG and JPEG2000-Based Dynamic Partial Reconfiguration on SOC for Remote Sensing Satellite On-Board Processing [Volume 7, Issue 1, 2014, Pages 57-66]

  • Chenarani, Hamed Velocity and Body Rate Control of a Spacecraft Using Robust Passivity-Based Control [Volume 11, Issue 2, 2018, Pages 41-46]

  • Chiniforoushan, Mohammad Model-Free Predictive Fault-Tolerant Control for Spacecraft Roto-Translational Relative Motion [Volume 14, Issue 1, 2021, Pages 77-92]

D

  • Dalir, Mohammad Ali GPS Signal Simulation in Intermediate Frequency (IF) [Volume 5, Issue 3, 2012, Pages 33-40]

  • Dameshghi, Adel Improving DGPS Accuracy Using Predictions of Reference Position Components Error Factors [Volume 8, Issue 2, 2015, Pages 41-56]

  • Daneshjoo, Kamran Identification of Space Deployable Mechanisms [Volume 9, Issue 3, 2016, Pages 53-71]

  • Daneshjoo, Z. Design and Aanalysis of Sandwich Panels as a Support Structure of Solar Cells for a GEO Communications Satellite [Volume 6, Issue 4, 2014, Pages 13-22]

  • Daneshnia, Ehsan Satellite Passes Simulation and Calculating the Satellite Rise and Set Times for the Site [Volume 5, Issue 4, 2013, Pages 29-38]

  • Daneshvar, Hamideh Study of Modeling Parameters in Determination of TID, DD, and SEE Radiation Damages for Satellite in LEO Orbit Using OMERE Software [Volume 12, Issue 3, 2019, Pages 63-71]

  • Daneshvar, Hamideh Analysis, Design and Optimization of the Multi Layer Radiation Shielding of Satellite Electronic Components [Volume 14, Issue 2, 2021, Pages 71-76]

  • Daneshvar, Hamideh Investigation and feasibility study of using components with different categories from the perspective of radiation damage in LEO and GEO orbits [Volume 14, Issue 4, 2021, Pages 11-23]

  • Daneshvar, Hamideh Experimental Study of the Effect of Using Space Sandwich Structures for Protection Against Space Radiation [Volume 15, Issue 2, 2022, Pages 59-69]

  • Daneshvar, Hamideh Investigating the Test and Evaluation of GaN Transistors Radiation Resistance in SSPA Amplifier Board in LEO Satellite Payload [Volume 16, Issue 1, 2023, Pages 59-74]

  • Darabi, H. Comparison Between Traditional Method (Statistical Method) and Multidisciplinary Optimization Method (AAO) in Designing of a Lightweight Liquid Propellant LV [Volume 5, Issue 1, 2012, Pages 61-72]

  • Darabi, Hossein Combining Gradient and Evolutionary Algorithms for Improving Collaborative Optimization Performance [Volume 8, Issue 2, 2015, Pages 27-39]

  • Dastoury, Hadi Multi-Disciplinary Optimization Conceptual Design of the Launcher Based on Non-Turbopump Propulsion Systems [Volume 15, Issue 1, 2022, Pages 121-137]

  • Davar, Ali Free Vibration Analysis of Grid Stiffened Doubly Curved Composite Shells Using a Refined Higher Order Theory [Volume 15, Issue 1, 2022, Pages 1-20]

  • Davari, Sajad Design and Simulation of Single Capillary Injector and Circular Injector Plate for a Monopropellant Thruster [Volume 15, Issue 3, 2022, Pages 109-118]

  • Davari, Sajjad Design and Configuration of Ground Sample Components of Low Propulsion Monopropellant Thruster Using Some Engineering Software [Volume 16, Issue 1, 2023, Pages 35-46]

  • Davari, Sajjad Optimized Dimension Design of Catalytic Chamber of a 10 N Thruster [Volume 16, Issue 2, 2023, Pages 55-61]

  • Davarnia, Ghazal Investigation of a Bi-propellant Thruster by a Developed Space Engine’s Thrust Chamber Analysis Code [Volume 14, Issue 2, 2021, Pages 47-37]

  • Davodi, A. Modeling and Control of Fuel Sloshing and its Effect on Spacecraft Attitude [Volume 11, Issue 4, 2018, Pages 11-22]

  • Dayyani, Abolfazl Study of Modeling Parameters in Determination of TID, DD, and SEE Radiation Damages for Satellite in LEO Orbit Using OMERE Software [Volume 12, Issue 3, 2019, Pages 63-71]

  • Dehghan, Seyed Mohammad Mehdi Satellite Spin Stabilization by Magnetic Torquers and Validation with Air-Bearing Simulator [Volume 9, Issue 2, 2016, Pages 25-34]

  • Dehghan, Seyed Mohammad Mehdi Evaluation of Magnetic Attitude control with Air-Bearing simulator [Volume 9, Issue 2, 2016, Pages 47-60]

  • Dehghan, S. M. Designing, Testing and Evaluation of Single Gimbal Control Moment Gyro for Microsatellite [Volume 2, Issue 1, 2009, Pages 13-23]

  • Dehghan, S. M. M. Implementation of Three Axis Attitude Controllers for Evaluation of a Micro-gravity Satellite Simulator [Volume 5, Issue 2, 2012, Pages 59-68]

  • Dehghan, S. M. M. Design, Manufacturing and Test of a Three Degrees-of-Freedom Attitude Control Simulator for an Agile Micro-Satellite Based on Single Gimbal Control Moment Gyros [Volume 7, Issue 3, 2014, Pages 51-67]

  • Dehghan, S. Mohammad Mahdi Satellite Passes Simulation and Calculating the Satellite Rise and Set Times for the Site [Volume 5, Issue 4, 2013, Pages 29-38]

  • Dehghan, S. Mohammad Mahdi Designing and Evaluation of an Experimental Attitude Determination System Using Sun Sensor and Magnetometer [Volume 5, Issue 4, 2013, Pages 69-78]

  • Dehghan, S.Mohammad Mehdi Sun Vector and Magnetic Vector Simulation for Hardware in the Loop Tests [Volume 10, Issue 1, 2017, Pages 47-53]

  • Dehghani, H. Multi-Receiver Modulation Classification for Satellite ommunications Signals [Volume 4, Issue 2, 2012, Pages 63-70]

  • Dehghani, H. SAR Imaging Systems Performance Modeling [Volume 6, Issue 1, 2013, Pages 47-56]

  • Dehghani, Hamid Design of a Multiband and Wide Angle Reflector [Volume 12, Issue 4, 2019, Pages 47-56]

  • Dehghani Mohammad-Abadi, Mohsen Approximate Solution of Required Velocity in Elliptical Earth Model Using Piecewise Linear [Volume 9, Issue 3, 2016, Pages 1-12]

  • Dehvari, Masoud The Retrieval of Wet Refractivity Index by Tomography Using Spherical Cap Harmonics [Volume 15, English Special Issue, 2022, Pages 15-24]

  • Dideban, Abbas A New Adaptive Controller for the Three ‎Axis Satellite Simulator Based on Continuous ‎Time Delay Petri Nets Tool [Volume 16, English Special Issue, 2023, Pages 25-38]

  • Doomiri Ganji, Davood Prediction of droplet size and velocity distribution based on maximum entropy formulation by nonlinear instability analysis of liquid sheet spray and turbulent of nozzle flow [Volume 13, Issue 1, 2020, Pages 1-11]

  • Doost, Roghayeh A Review of the Applications of Artificial Intelligence in Improving the Performance of Integrated Space-Air and Ground Networks [Volume 16, Issue 2, 2023, Pages 27-42]

  • Doost, Roghayeh Determining Allowed Positions of Aeronautical-Earth Station in Motion (A-ESIM) Prevent its Frequency Interference in the Fixed Ground Station [Volume 16, Issue 3, 2023, Pages 1-14]

  • Doustdar, Mohammad Mehdi Investigation the effect of flameholder on the combustion chamber performance of a ramjet engine [(Articles in Press)]

E

  • Ebrahimi, A. Optimal Control of Low Propulsion Orbital Transfer Time [Volume 4, Issue 1, 2011, Pages 23-28]

  • Ebrahimi, Ahmad The Turbulence Model in the Spacecraft by using A Moving Pulsed Ball Model [Volume 14, Issue 3, 2021, Pages 15-22]

  • Ebrahimi, Asghar Robust Guidance Algorithmfor Reentry Vehicles based on PLS Regression in the Presence ofInitail Parameter Uncertainties [Volume 10, Issue 4, 2018, Pages 29-40]

  • Ebrahimi, Asghar Nonlinear Optimal Control of Reentry Vehicles Based on Deriving the State and Control Depended Systematic Matrices in State Space Form [Volume 11, Issue 1, 2018, Pages 1-12]

  • Ebrahimi, M. Multidisciplinary Design Optimization of a Small Launch Vehicle; a System Sensitivity Analysis Approach [Volume 1, Issue 1, 2008, Pages 47-56]

  • Ebrahimi, M. کاربرد مدل پاندول ساده به منظور اعمال دینامیک تلاطم سیال در شبیه‌سازی شش درجه آزادی پرواز ماهواره‌بر [Volume 3, Issue 2, 2011, Pages 59-67]

  • Ebrahimi, M. Survey on Nondeterministic Optimal Design and Its Applications in the Aerospace Industry [Volume 4, Issue 2, 2012, Pages 23-34]

  • Ebrahimi, M. The Study of Hypergravity and Flight Stress on Different Cell Lines Function in Sounding Rocket [Volume 6, Issue 4, 2014, Pages 37-42]

  • Ebrahimi, M. Study of Recovery System Performance of a Sounding Rocket using Launching Tests [Volume 7, Issue 2, 2014, Pages 23-33]

  • Ebrahimi, Masoud Star Catalog Criteria Selection and Mission Catalog Update for a Typical Star Tracker [Volume 5, Issue 4, 2013, Pages 1-8]

  • Ebrahimi, Masoud Robust Switching Surfaces Sliding Mode Guidance for Terminal Rendezvous in Near Circular Orbit [Volume 11, Issue 2, 2018, Pages 21-31]

  • Ebrahimi, Mohammad Experimental Analysis of Pyroshock Wave Propagation in Kavoshgar's Payload [Volume 7, Issue 4, 2015, Pages 51-62]

  • Ebrahimi, Mohammad Aerodynamic Heating Prediction of Flying Body Using Fluid-Solid Conjugate Heat Transfer [Volume 8, Issue 3, 2015, Pages 41-53]

  • Ebrahimi, Mohsen Bearing only Tracking for Maneuver Target using Nonlinear Second-Order Markov Model [Volume 15, Issue 3, 2022, Pages 11-22]

  • Ebrahimi, R. An Investigation on the Effect of Chemical Kinetics Mechanisms in the Modeling of Combustive Gaseous Oxidizer Flow on a Solid Fuel Surface [Volume 3, Issue 1, 2010, Pages 1-13]

  • Ebrahimi, R. Modeling of Shutdown Process in Liquid Propellant Rocket Engines [Volume 6, Issue 4, 2014, Pages 1-11]

  • Ebrahimik, Masoud Improvement of the Electrical Potential Distribution on the Surface Geostationary Satellites using Material Change [Volume 10, Issue 3, 2017, Pages 25-39]

  • Ebrahimi Kachoei, Masoud Visual-Inertial Navigation System based on a New approach in Tracking and Investigating the Image Feature Points [Volume 12, Issue 3, 2019, Pages 43-54]

  • Ebrahimi Kachoie, Masoud A Survey on Vision Navigation Methods for UAV Navigation Applications [Volume 10, Issue 2, 2017, Pages 33-52]

  • Ebrahimi Kachouie, Masoud Consideration on Actualizing the Non-Dimensional Star Pattern Recognition Algorithm for a Typical Laboratory Star Tracker [Volume 5, Issue 2, 2012, Pages 15-23]

  • Edalatpour, Amirhossein Performance Analysis of Liquid Propellant Micro-propulsion with Liquid Oxygen as Cryogenic Oxidizer [Volume 12, Issue 1, 2019, Pages 23-40]

  • Eftekhari, Hossein Scientometric analysis of published scientific productions in the field of satellite constellations [(Articles in Press)]

  • Ehyaei, Amir Farhad Bearing only Tracking for Maneuver Target using Nonlinear Second-Order Markov Model [Volume 15, Issue 3, 2022, Pages 11-22]

  • Eidi, Azam Investigation and feasibility study of using components with different categories from the perspective of radiation damage in LEO and GEO orbits [Volume 14, Issue 4, 2021, Pages 11-23]

  • Eidi, Azam Using Space Radiation Shielding Made of Polyethylene Instead of Aluminum in GEO Orbit to Reduce Weight [Volume 16, Issue 4, 2023, Pages 15-27]

  • EidiAttarZade, Masoud Investigation of a Bi-propellant Thruster by a Developed Space Engine’s Thrust Chamber Analysis Code [Volume 14, Issue 2, 2021, Pages 47-37]

  • Eidi Esfiani, Nahid Using Space Radiation Shielding Made of Polyethylene Instead of Aluminum in GEO Orbit to Reduce Weight [Volume 16, Issue 4, 2023, Pages 15-27]

  • Elahian, Samaneh Collision Prediction of Spacecraft for Space Traffic Management [Volume 15, Issue 2, 2022, Pages 93-102]

  • Emadi Noori, Yazdan Integrated Design of Orbital Transfer Block in an Optimized and Multistep Converged Environment [Volume 7, Issue 4, 2015, Pages 23-37]

  • Emami, R. Developing Attitude Control for Suborbital Module Based on Cold Gas Thrusters and Using Quaternion Feedback [Volume 6, Issue 1, 2013, Pages 1-10]

  • Emami, R. Satellite Conceptual Design Multi-Objective Optimization Using Co Framework [Volume 7, Issue 1, 2014, Pages 1-12]

  • Emami, Shiva The presentation of the ARTA CanSat design and construction process at the CANSAT International Competition in Iran [Volume 13, Issue 2, 2020, Pages 63-77]

  • Emami, Shiva Thermal Modeling of Lidar Payload in a Remote Sensing Satellite under System Level Considerations with a Review on its Challenges [Volume 16, Issue 2, 2023, Pages 79-91]

  • Eshagh nia, Hanieh The presentation of the ARTA CanSat design and construction process at the CANSAT International Competition in Iran [Volume 13, Issue 2, 2020, Pages 63-77]

  • Eshaghnia, Hanieh Performance evaluation of a launch vehicle with non-turbopump propulsion system based on multidisciplinary analysis (MDA) [Volume 14, Issue 4, 2021, Pages 35-49]

  • Eshaghnia, Hanieh Multi-Disciplinary Optimization Conceptual Design of the Launcher Based on Non-Turbopump Propulsion Systems [Volume 15, Issue 1, 2022, Pages 121-137]

  • Eshaghnia, Hanieh Introducing the conceptual design process of the Armita lunar rover Based on ECSS [(Articles in Press)]

  • Eskandari, Afshin Design and Optimization of Satellite Telecommunication Relay Using Pseudo-Noise Ranging [Volume 15, Issue 4, 2022, Pages 45-56]

  • Eskandari, Mohammad Amin Dynamic & Non-linear Modelling of an Expansion Cycle Rocket Engine [Volume 13, Issue 1, 2020, Pages 39-48]

  • Eskandari Jam, J. Governing Equations in Mechanical Analysis of Satellite Carrier Adapter [Volume 5, Issue 1, 2012, Pages 41-50]

  • Eskandari Jam, Jafar Free Vibration Analysis of Grid Stiffened Doubly Curved Composite Shells Using a Refined Higher Order Theory [Volume 15, Issue 1, 2022, Pages 1-20]

  • Eskandari Shahraki, Majid Free Vibration Analysis of Grid Stiffened Doubly Curved Composite Shells Using a Refined Higher Order Theory [Volume 15, Issue 1, 2022, Pages 1-20]

  • Eslami, A. A. Reliability Determination of a Sounding Rocket Separation System Using its Reliability Block Diagram and FMEA [Volume 7, Issue 1, 2014, Pages 25-31]

  • Eslami Mehrjardi, Amir Design of an Attitude Control and Power Management System for a Remote Sensing Satellite Considering of Reaction Wheels Saturation Effects [Volume 5, Issue 4, 2013, Pages 39-45]

  • Esmaeelzade, M. Analysis of Navid Satellite TLE Data and it’s Effects on Tracking Operations by the Ground Stations [Volume 6, Issue 2, 2013, Pages 29-42]

  • Esmaeili, Mostafa Numerical Simulation of Turbulent Reacting flow in a Trapped Vortex Combustor [Volume 10, Issue 1, 2017, Pages 15-25]

  • Esmaeili, Mostafa Numerical Simulation and Optimization of Forced Convection Heat Transfer of Magnetic Nanofluid in a Channel in the Presence of a Non-Uniform Magnetic Field [Volume 11, Issue 2, 2018, Pages 11-19]

  • Esmaeilian, A. Studying and Calculating the Radiation Damage Caused by the Solar Radiation Spectrum in the Crystal Structure of Semiconductor Components [Volume 6, Issue 3, 2013, Pages 55-60]

  • Esmaeilzadeh, M. Increasing Accuracy of Satellite Position Prediction with Considering Harmonics of Potential Function of the Earth [Volume 6, Issue 3, 2013, Pages 27-37]

  • Esmaeilzadeh, Majed Introduction to Tadbir satellite Orbit Determination System [Volume 8, Issue 3, 2015, Pages 65-70]

  • Esmaeilzadeh, Seyed Majid (Technical Note) Design and Construction of Star Tracker Platform in Order to Satellite Attitude Determination Based on Star Tracking Algorithm [Volume 9, Issue 2, 2016, Pages 85-90]

  • Esmaelzadeh, R. Explicit Flatness-Based Guidance in Reentry Phase [Volume 6, Issue 4, 2014, Pages 29-36]

  • Esmaelzadeh, Reza Flatness-based Near Optimal Guidance [Volume 10, Issue 3, 2017, Pages 15-24]

  • Esmaili, Mostafa Numerical Simulation of Sloshing in a Container under Translational and Angular Accelerations [Volume 10, Issue 2, 2017, Pages 9-21]

  • Etemadi, Fskhri Aerodynamic Heating Prediction of Flying Body Using Fluid-Solid Conjugate Heat Transfer [Volume 8, Issue 3, 2015, Pages 41-53]

F

  • Fadakar, Elyas Optimal Mission Design for Moon Exploration Expedition [Volume 11, Issue 2, 2018, Pages 47-53]

  • Fahami, M. GPS Radio Occultation Method for Ionosphere TEC Monitoring [Volume 6, Issue 2, 2013, Pages 21-28]

  • Fakhri, M. Development of an Integrated Design Environment for Optimal Ascent Trajectory Planning [Volume 1, Issue 1, 2008, Pages 1-10]

  • Fakoor, M. Hybrid Estimation of Gyro Model Parameters and GEO Satellite Moment of Inertia with Extended Kalman Filter [Volume 6, Issue 2, 2013, Pages 67-74]

  • Fakoor, M. Design and Aanalysis of Sandwich Panels as a Support Structure of Solar Cells for a GEO Communications Satellite [Volume 6, Issue 4, 2014, Pages 13-22]

  • Fakoor, Mahdi Uncertainty approach in layout design of satellite subsystems considering natural frequency constraints [Volume 14, Issue 1, 2021, Pages 65-75]

  • Fallah-Pour, M. B. SAR Imaging Systems Performance Modeling [Volume 6, Issue 1, 2013, Pages 47-56]

  • Fani Saberi, Farhad Design of an Attitude Control and Power Management System for a Remote Sensing Satellite Considering of Reaction Wheels Saturation Effects [Volume 5, Issue 4, 2013, Pages 39-45]

  • Fani Saberi, Farhad Design and Implementation of Backstepping-Sliding mode Attitude Controller in The Prossecor in The Loop Test Bed [Volume 9, Issue 1, 2016, Pages 25-35]

  • Fani Saberi, Farhad Satellite Adaptive Attitude Control Based on Decentralized Minimal Control in the Presence of Reaction wheel Accurate Model [Volume 9, Issue 1, 2016, Pages 47-56]

  • Fani Saberi, Farhad Adaptive Generalized-Minimum-Variance Attitude Control of a High Pointing-Accuracy Remote Sensing Satellite [Volume 16, English Special Issue, 2023, Pages 1-23]

  • Fani Saberi, Farhd Design and Implementation of Attitude Control Systemof a satellite with Stereo-Imaging Scenario in Hardware in the Loop Test Bed [Volume 8, Issue 3, 2015, Pages 15-26]

  • Fani- Saberi, F. Design of an Attitude Control System for a Stereo-Imagery Satellite with Combining of Along-Track and Across-Track Configurations [Volume 1, Issue 2, 2008, Pages 9-15]

  • Fani- Saberi, F. Design of Attitude Control System of an Axisymmetric Satellite with Gravity Gradient Stabilization and Slow Spinning about Yaw Axis [Volume 1, Issue 2, 2008, Pages 27-33]

  • Fani-Saberi, F. Design of an Attitude Estimation Algorithm for a LEO Satellite Based on Multiple Models Adaptive Method and Comparison with EKF [Volume 2, Issue 2, 2009, Pages 17-26]

  • Farajollahi, Amirhamzeh Numerical Study on the Effects of Nozzle Geometry and Creating Swirly Flow Inside the Injector Nozzle on the Performance of an Engine [Volume 15, Issue 4, 2022, Pages 107-121]

  • Farajollahi, Hossein Isolation of Satellite's Sensitive Equipments from Longitudinal Vibration of Launch Vehicle Using Silicone Gel [Volume 7, Issue 4, 2015, Pages 81-91]

  • Farhang, M. Multi-Receiver Modulation Classification for Satellite ommunications Signals [Volume 4, Issue 2, 2012, Pages 63-70]

  • Farhang Laleh, Farhad Design and Fabrication of Spool Type Pin Puller Mechanism- from Concept to Qualification Model [Volume 9, Issue 3, 2016, Pages 37-51]

  • Farhani, F. Determination of Deployment Angle for the Optimum Operation of Solar Panels Used in a LEO Satellite [Volume 1, Issue 2, 2008, Pages 1-8]

  • Farhani, F. Effects of Some Parameters on Thermal Control of a LEO Satellite [Volume 7, Issue 1, 2014, Pages 13-24]

  • Farokhi, R. Neural Network Based Diagnostic Indication of a Liquid Propellant Engine with Faulty Data Collection System [Volume 7, Issue 2, 2014, Pages 75-83]

  • Farrokhi, R Study of Hot Gas Pressurizing System Tank and Liquid Rocket Engine Interaction by Dynamic Simulation [Volume 6, Issue 1, 2013, Pages 11-19]

  • Farrokhi, R. Dynamics Simulation of Pressurizing in Propulsion System Configuration [Volume 6, Issue 3, 2013, Pages 1-13]

  • Farshchi, M. Design and Manufacturing a Laboratory Example of Pulsed Plasma Thruster [Volume 3, Issue 2, 2011, Pages 23-30]

  • Farshchi, Mohammad Numerical Investigation of Laminar Premixed Conical Flame Response to Acoustic Excitation [Volume 8, Issue 1, 2015, Pages 9-18]

  • Farshchi, Mohammad Investigation of a Bi-propellant Thruster by a Developed Space Engine’s Thrust Chamber Analysis Code [Volume 14, Issue 2, 2021, Pages 47-37]

  • Farsi, M. A. Investigation and Analysis of Seperation System of Kavoshgar-3 [Volume 3, Issue 1, 2010, Pages 15-23]

  • Farsi, M. A. Reliability Determination of a Sounding Rocket Separation System Using its Reliability Block Diagram and FMEA [Volume 7, Issue 1, 2014, Pages 25-31]

  • Farsi, M. A. Study of Recovery System Performance of a Sounding Rocket using Launching Tests [Volume 7, Issue 2, 2014, Pages 23-33]

  • Farsi, Mohammad Ali Experimental Analysis of Pyroshock Wave Propagation in Kavoshgar's Payload [Volume 7, Issue 4, 2015, Pages 51-62]

  • Farsi, Mohammad Ali Thermal Effects of the Space Environment on the Radiation Characteristics of a Reflector Antenna in LEO Satellite [Volume 15, Issue 2, 2022, Pages 103-113]

  • Faryadi, S. Remote Sensing Role in Land Use StudiesCase Study: Tehran Metropolitan and its Boundary [Volume 7, Issue 3, 2014, Pages 69-73]

  • Farzaneh, Saeed The Retrieval of Wet Refractivity Index by Tomography Using Spherical Cap Harmonics [Volume 15, English Special Issue, 2022, Pages 15-24]

  • Fasooniehch, A.R. Evaluation of the Effects of Radiation, Irradiance, and Temperature on Solar Cell Electrical Characteristics and Extraction of Maximum Solar Panel Power by MPPT [Volume 1, Issue 1, 2008, Pages 67-80]

  • Fatehi, Mohammad Maximum Likelihood-Based Worst-Case Optimization Design of Hydrazine Propulsion System for aSatellite Orbital Transfer System under Uncertainty [Volume 14, Issue 3, 2021, Pages 1-14]

  • Fatehi, Mohammad Fatehi Design of an Upper Stage Propulsion System by Multi Objective Hybrid PSO [Volume 13, Issue 3, 2020, Pages 1-16]

  • Fathi, Alireza Numerical Modeling of plasma flow in an Electrohydrodynamic thruster with two-cathode electrode arrangement [Volume 12, Issue 2, 2019, Pages 1-10]

  • Fathi, Mehdi INS Alignment Improvement Using Rest Heading and Zero-Velocity Updates [Volume 8, Issue 4, 2016, Pages 45-51]

  • Fathi, Mohammad Extensive Regional Telecommunications Coverage in Emergency Condition Using Tethered-Balloon Equipped with Antenna Pointing Mechanism – Part 1: Kinematic and Dynamic Modeling [Volume 15, Issue 2, 2022, Pages 27-41]

  • Fathi, Mohammad Extensive Regional Telecommunications Coverage in Emergency Condition Using Satellite and Tethered-Balloon Equipped with Antenna Pointing Mechanism – Part 2: Operation Modes and Controller Design [Volume 15, Issue 4, 2022, Pages 71-88]

  • Fathi, Mohsen Design a μ-Controller ToControl Attitude of a Flexible Microsatellite [Volume 8, Issue 1, 2015, Pages 61-71]

  • Fayazbakhsh, H. R. Optimal Control of Low Propulsion Orbital Transfer Time [Volume 4, Issue 1, 2011, Pages 23-28]

  • Fazeli, H. Comprehensive Pattern in Designing Low-Thrust Space Propulsion Systems [Volume 7, Issue 3, 2014, Pages 9-21]

  • Fazeli, Hamid Experimental Study of Dynamic Stability for a Entry Capsule in Supersonic Flow [Volume 15, Issue 2, 2022, Pages 71-80]

  • Fazelzadeh, S. A. Optimal Low-Thrust Spacecraft Trajectories Using Time-Domain Finite Element Method [Volume 1, Issue 2, 2008, Pages 43-50]

  • Fazelzadeh, Seyed Ahmad Active Control of a Smart Satellite under Thermal Loading [Volume 8, Issue 1, 2015, Pages 43-51]

  • Fazlyab, Alireza Design and Implementation of Backstepping-Sliding mode Attitude Controller in The Prossecor in The Loop Test Bed [Volume 9, Issue 1, 2016, Pages 25-35]

  • Feghhi, S. A. Measurement of Neutron Irradiation Effect on Reverse Current Damage Constant α for Diode [Volume 6, Issue 2, 2013, Pages 11-19]

  • Feghhi, S. A. H Studying and Calculating the Radiation Damage Caused by the Solar Radiation Spectrum in the Crystal Structure of Semiconductor Components [Volume 6, Issue 3, 2013, Pages 55-60]

  • Feghhi, S. A. H. Sensitive Volume Modeling in Calculation of Space Radiation-Induced SEU Cross Section [Volume 6, Issue 4, 2014, Pages 23-28]

  • Feghhi, S. Amir Hossein Calculation and measurement of leakage current variations due to displacement damage for a silicon diode exposed to space protons [Volume 13, Issue 4, 2020, Pages 71-79]

  • Feghhi, S. Amir Hossein Studying the Effects of Multi-Layer Shielding in Reducing Space Radiations Exposure of Human and Electrical Components in Space Missions [Volume 16, Issue 2, 2023, Pages 19-26]

  • Feghhi, Seyed Amir Hossein Using Space Radiation Shielding Made of Polyethylene Instead of Aluminum in GEO Orbit to Reduce Weight [Volume 16, Issue 4, 2023, Pages 15-27]

  • Firuzi, Reza Numerical Study on the Effects of Nozzle Geometry and Creating Swirly Flow Inside the Injector Nozzle on the Performance of an Engine [Volume 15, Issue 4, 2022, Pages 107-121]

  • Fiuzy, Mohammad (Technical Note) Design and Construction of Star Tracker Platform in Order to Satellite Attitude Determination Based on Star Tracking Algorithm [Volume 9, Issue 2, 2016, Pages 85-90]

  • Foroughi, Mahdi Design and Real-time Implementation of the Adaptive-Neuro-Fuzzy Controller for a Temperature Control System using Model-Based Design [Volume 10, Issue 4, 2018, Pages 9-17]

  • Fouladi, Nourbakhsh Developing a Universal Software for the Conceptual Design of Cryogenic Rocket Propulsion System [Volume 15, Issue 1, 2022, Pages 73-87]

G

  • Garshasbi-Nia, N. Governing Equations in Mechanical Analysis of Satellite Carrier Adapter [Volume 5, Issue 1, 2012, Pages 41-50]

  • Gazerpour, Hamid Orbit Determination via a Deeply- Coupled UKF/GNSS Filter [Volume 9, Issue 3, 2016, Pages 13-26]

  • Ghaderi-Dehkordi, Y. Design and Fabrication of Protective Corrugated Tunnels for Using in Aerospace Structures [Volume 2, Issue 3, 2009, Pages 27-34]

  • Ghaderi-Dehkordi, Y. Investigation of the Effect of Reinforcement on Thermo-Physical Properties of Ablative Heat Shields [Volume 3, Issue 1, 2010, Pages 55-65]

  • Ghadiri Massoom, Nooredin Investigation on Performance Characteristics of Hydrazine Monopropellant Thruster according to Reaction Chamber Adiabatic Temperature [Volume 15, Issue 3, 2022, Pages 33-47]

  • Ghafari, A. Flexible Spacecraft Attitude Control using Hybrid Control Scheme of H∞ and Sliding Mode Control [Volume 1, Issue 2, 2008, Pages 51-56]

  • Ghafari, A. Flexible Spacecraft Three Axis Attitude Maneuver by Active Vibration Control [Volume 2, Issue 1, 2009, Pages 43-50]

  • Ghafary, B Electro-Optical Design of Imaging Payload for a Remote Sensing Satellite [Volume 2, Issue 3, 2009, Pages 57-70]

  • Ghaffari, M. R. 3D Modeling of Ionospheric Tomography Using GPS Observations Geodynamics Network of Iran in Three Different Seasons [Volume 4, Issue 1, 2011, Pages 1-14]

  • Ghaffari, Valiollah Performance and Stability Investigation of a line of sight based Guidance System in the Presence of Measurement Noise [Volume 11, Issue 1, 2018, Pages 31-40]

  • Ghaffari Razin, Mir Reza Time series modeling of ionosphere total electron content using wavelet neural network and hybrid PSO training algorithm [Volume 13, Issue 3, 2020, Pages 39-50]

  • Ghaffari-Razin, Seyyed Reza Efficiency of the least squares support vector regression in local modeling of the ionosphere total electron content and comparison with other models [Volume 17, Issue 1, 2024, Pages 21-36]

  • Ghahramani, Mohammad Design and Fabrication of Spool Type Pin Puller Mechanism- from Concept to Qualification Model [Volume 9, Issue 3, 2016, Pages 37-51]

  • Ghahramani, Nemat Ollah INS Alignment Improvement Using Rest Heading and Zero-Velocity Updates [Volume 8, Issue 4, 2016, Pages 45-51]

  • Ghanbari, H. Attitude Control of Spacecraft Using L1 Adaptive Control in the Presence of Actuator and Disturbances [Volume 13, Issue 2, 2020, Pages 79-86]

  • Ghanbarian, A. Considerations of Utilizing Telemetry and GPS System in Sounding Rockets [Volume 1, Issue 1, 2008, Pages 81-86]

  • Ghanbarpoor, H. Automatic Star Identification Using Triangle Base and Increase Search Speed [Volume 4, Issue 2, 2012, Pages 83-92]

  • Gharezi, Sajjad Investigation the effect of flameholder on the combustion chamber performance of a ramjet engine [(Articles in Press)]

  • Ghasemi, Hojat Design, Fabrication, and Test of a Cryogenic Liquid Oxygen-Ethanol Engine [Volume 16, Issue 1, 2023, Pages 47-58]

  • Ghasemloo, S. Approximate Viscous Shock-Layer Analysis of Axisymmetric Bodies in Perfect Gas Hypersonic Flow [Volume 7, Issue 1, 2014, Pages 41-48]

  • Ghasemmi, H. Numerical Simulation of Complicated Grain Burnback in Three Dimensions [Volume 5, Issue 1, 2012, Pages 15-28]

  • Ghasrizadeh, Reza improve coarse alignment in inertial navigation system By the method of Identification the Kalman filter matrix [Volume 13, Issue 4, 2020, Pages 81-90]

  • Ghasrizadeh, Reza Improved Spoofing Loosely Coupled INS /GPS with ‎Steady State Kalman Matrix Gain [Volume 16, Issue 3, 2023, Pages 37-49]

  • Ghassemi, Hojat Design, Manufacture and Experimental Study of a Hydrogen Peroxide-HTPB Hybrid Rocket Motor [Volume 5, Issue 4, 2013, Pages 19-28]

  • Ghazanfarinia, Sajjad Thermal Modeling of Lidar Payload in a Remote Sensing Satellite under System Level Considerations with a Review on its Challenges [Volume 16, Issue 2, 2023, Pages 79-91]

  • Ghazanfarinia, Sajjad Economic analysis of exploitation of lunar resources [(Articles in Press)]

  • Ghedamini Harouni, amirreza Multidisciplinary optimization for configuration of a reentry capsule considering uncertainty [Volume 12, Issue 4, 2019, Pages 1-17]

  • Gheisari, M.M. Second Order Level Set Method in Numerical Simulation of the Grain Burn-Back [Volume 7, Issue 3, 2014, Pages 23-32]

  • Ghobadi, M. Optimal Control of a Tri-axial Spacecraft Simulator Test bed Actuated by Reaction Wheels [Volume 8, Issue 4, 2016, Pages 35-44]

  • Ghobadi, Mahdi Control Allocation for Redundant Thruster of a Spacecraft via Direction-Preserving Approach in Simplex Algorithm [Volume 13, Issue 1, 2020, Pages 71-82]

  • Gholami, Mahdi Space Industry Funding: Public and Private sector [Volume 14, Issue 4, 2021, Pages 67-76]

  • Gholami Mazinan, H. Designing an Estimation Pattern for Reliability of Launch Vehicle Structure with Bayesian Networks [Volume 5, Issue 1, 2012, Pages 73-80]

  • Ghorbani, Ramin Implementation of Developing Linear Hydrodynamic Instability Theory on a Hollow Cone-shaped Liquid Sheet of a Swirl Injector [Volume 11, Issue 4, 2018, Pages 1-10]

  • Ghorbani Vaghei, B. Design of Attitude Control System of an Axisymmetric Satellite with Gravity Gradient Stabilization and Slow Spinning about Yaw Axis [Volume 1, Issue 1, 2008, Pages 11-19]

  • Ghorbani Vaghei, Bahman The magnetic cleanliness of a satellite Based on optimum placement of equipment using PSO [Volume 14, Issue 2, 2021, Pages 61-69]

  • Ghorbani-Vaghei, B. Design of an Attitude Control System for a Stereo-Imagery Satellite with Combining of Along-Track and Across-Track Configurations [Volume 1, Issue 2, 2008, Pages 9-15]

  • Ghorbani-Vaghei, B. Design of Attitude Control System of an Axisymmetric Satellite with Gravity Gradient Stabilization and Slow Spinning about Yaw Axis [Volume 1, Issue 2, 2008, Pages 27-33]

  • Ghorbani Vagheii, B. Satellite Camera CCD Read-out System Design, Based on Noise Optimization with Respect to Satellite Limitations [Volume 2, Issue 3, 2009, Pages 19-26]

  • Ghorbani Vagheii, B. A Spin Satellite Imaging System Design with Real Time Imaging Capability Using FPGA [Volume 3, Issue 1, 2010, Pages 45-54]

  • Ghorbany Vagheii, B. Satellite Thermal Modeling and Analysis with the Electrical Network Method [Volume 5, Issue 1, 2012, Pages 81-90]

  • Ghorbi, Mohammad Effect of Injector Pressure Drop on The ‎Performance of A 1 N Monopropellant ‎Thruster [Volume 15, Issue 4, 2022, Pages 19-29]

  • Ghordoyi Milan, Kavoos Analysis, Design and Optimization of the Multi Layer Radiation Shielding of Satellite Electronic Components [Volume 14, Issue 2, 2021, Pages 71-76]

  • Giyome- Bozorgi, S. Javad Space Application of a Linear Array of Plasma Antenna [Volume 5, Issue 3, 2012, Pages 59-66]

  • Gohari, Seyyed Amir Design, Simulation, Fabrication and Determining the Equivalent Circuit Model of a Reconfigurable FSS unit Cell Filter for Electromagnetic Protection of Space Payload Systems [Volume 16, Issue 4, 2023, Pages 71-82]

  • Goharkhah, Mohmmad Numerical Simulation and Optimization of Forced Convection Heat Transfer of Magnetic Nanofluid in a Channel in the Presence of a Non-Uniform Magnetic Field [Volume 11, Issue 2, 2018, Pages 11-19]

  • Golro, Ali Akbar Role of States in Regulating Space Activities in International Law [Volume 9, Issue 4, 2017, Pages 27-37]

  • Golroo, A.A. Process of Liability Principles in International Space Law [Volume 5, Issue 2, 2012, Pages 35-48]

  • Gorgin, R. Reliability Determination of a Sounding Rocket Separation System Using its Reliability Block Diagram and FMEA [Volume 7, Issue 1, 2014, Pages 25-31]

  • Gorji, A.M. Investigation of Length and Velocity Variation Effects on Unsteady Separation of Parallel Boosters [Volume 7, Issue 2, 2014, Pages 49-61]

H

  • Habiba, Saeed The Intellectual Property Rights and Transfer of Technology in Space Industry [Volume 15, Issue 1, 2022, Pages 107-119]

  • Habibi, Mona Uncertainty approach in layout design of satellite subsystems considering natural frequency constraints [Volume 14, Issue 1, 2021, Pages 65-75]

  • HadiDoolabi, M. Investigation of Length and Velocity Variation Effects on Unsteady Separation of Parallel Boosters [Volume 7, Issue 2, 2014, Pages 49-61]

  • Haghi, H. Optimal Control of a Tri-axial Spacecraft Simulator Test bed Actuated by Reaction Wheels [Volume 8, Issue 4, 2016, Pages 35-44]

  • Haghighat Esfahani, Mahmood Applying a Novel Comprehensive Preference-based Design (CPD) Approach to Conceptual Design of Space Transportation System [Volume 14, Issue 3, 2021, Pages 39-50]

  • Haghighi, Hosein Design and implementation of hardware-in-the-loop (HIL) test-bed for spacecraft attitude control [Volume 12, Issue 2, 2019, Pages 55-70]

  • Haghighi, Hossein Damping mode of satellite angular velocity using magnetic actuators in hardware/software in the loop [Volume 12, Issue 4, 2019, Pages 57-67]

  • Haghparast, M. Design of Fault Detection, Identification and Recovery Algorithms for a 3-Axis Stabilized Satellite [Volume 5, Issue 1, 2012, Pages 29-40]

  • Haghparast, M. Design of Adaptive Threshold Based Fault Detection and Isolation for Attitude Control System of a Three Axis Satellite [Volume 6, Issue 1, 2013, Pages 31-46]

  • Haghparast, M. Increasing Accuracy of Satellite Position Prediction with Considering Harmonics of Potential Function of the Earth [Volume 6, Issue 3, 2013, Pages 27-37]

  • Haghshenas, Javad Modeling and calculating the albedo and IR heat flux applied to satellite based on the geographic position of sarellite [Volume 11, Issue 4, 2018, Pages 23-30]

  • Haghshenas, Javad High Precision Remote Sensing Payload Alignment Procedure Using Theodolite and Alignment Cube [Volume 16, Issue 1, 2023, Pages 1-9]

  • Haghshenas, Javad Star Sensor Relative Accuracy Measurement in Night Sky [Volume 13, Issue 3, 2020, Pages 79-89]

  • Hajati, Bahar The comparison of the binding parameters of silver nanoparticles to DNA in gravity and microgravity conditions [Volume 13, Issue 1, 2020, Pages 61-70]

  • Hajebrahimi, Z. The Study of Hypergravity and Flight Stress on Different Cell Lines Function in Sounding Rocket [Volume 6, Issue 4, 2014, Pages 37-42]

  • Hajebrahimi, Zahra The Effects of Simulated Microgravity on Serum Levels of VEGF in Male Wistar Rats [Volume 9, Issue 4, 2017, Pages 63-68]

  • Hajebrahimi, Zahra Evaluation of RKIP gene expression changes of MDA-MB-231 breast cancer cell line after microgravity treatment [Volume 12, Issue 1, 2019, Pages 69-76]

  • Hajebrahimi, Zahra CD44 expression changes in MDA-MB-231 cell line of breast cancer after exposure to 2-D clinorotation [Volume 14, Issue 4, 2021, Pages 61-66]

  • Hajebrahimi, Zahra Effect of Simulated Microgravity Condition on Cells Proliferation and Myostatin Gene Expression in Differentiated Skeletal Muscle Cells (C2C12) [Volume 15, Issue 2, 2022, Pages 81-92]

  • Hajebrahimi, Zahra The comparison of the binding parameters of silver nanoparticles to DNA in gravity and microgravity conditions [Volume 13, Issue 1, 2020, Pages 61-70]

  • Hajebrahimi, Zahra E-cadherin gene expression changes in MCF-7 breast cancer cell line in simulated microgravity condition [(Articles in Press)]

  • Hajebrahimi, Zahrs Study of the Effect of the Microgravity on the Expression of Angiogenesis Marker in Endothelial Progenitor Cells [Volume 15, Issue 4, 2022, Pages 89-96]

  • Haji Jafari, Mohammad Structural Design Modification of a CubeSat Regarding Modal Compatibility for Launching by Vega C Launcher [Volume 16, Issue 4, 2023, Pages 41-56]

  • Hajipour, Pedram Investigation and feasibility study of using components with different categories from the perspective of radiation damage in LEO and GEO orbits [Volume 14, Issue 4, 2021, Pages 11-23]

  • Hajipour, Pedram A Review of the Applications of Artificial Intelligence in Improving the Performance of Integrated Space-Air and Ground Networks [Volume 16, Issue 2, 2023, Pages 27-42]

  • Hajipour, Pedram Determining Allowed Positions of Aeronautical-Earth Station in Motion (A-ESIM) Prevent its Frequency Interference in the Fixed Ground Station [Volume 16, Issue 3, 2023, Pages 1-14]

  • Hajipour, Pedram Using Space Radiation Shielding Made of Polyethylene Instead of Aluminum in GEO Orbit to Reduce Weight [Volume 16, Issue 4, 2023, Pages 15-27]

  • Hajipour, Pedram Scientometric analysis of published scientific productions in the field of satellite constellations [(Articles in Press)]

  • Hamedi, mohammad hadi 2D Simulation of Designed Dual Throat Nozzle using Geometrical Analogy [Volume 10, Issue 2, 2017, Pages 23-32]

  • Hamrah, R. Modeling of Space Objects Propagation, Prediction of Closest Approaches among Satellites, and Assessment of Maximum Collision Probability [Volume 6, Issue 1, 2013, Pages 57-67]

  • Hasani, S. Mehdi Consideration on Actualizing the Non-Dimensional Star Pattern Recognition Algorithm for a Typical Laboratory Star Tracker [Volume 5, Issue 2, 2012, Pages 15-23]

  • Hashemi, Davood Design a Model of Four Color Separation Prism in Satellite Camera [Volume 5, Issue 3, 2012, Pages 41-48]

  • Hashemi, Malihe (Technical Note) Design and Construction of Star Tracker Platform in Order to Satellite Attitude Determination Based on Star Tracking Algorithm [Volume 9, Issue 2, 2016, Pages 85-90]

  • Hashemi Doulabi, S. M. Comparison Between Traditional Method (Statistical Method) and Multidisciplinary Optimization Method (AAO) in Designing of a Lightweight Liquid Propellant LV [Volume 5, Issue 1, 2012, Pages 61-72]

  • Hashemi Mehne, Seyed Hamed Review of a Swirl Double Base Injector Performance by It’s Hot-Fire Test on a Laboratory Liquid Micro Impulse Engine With Single Injector [Volume 9, Issue 1, 2016, Pages 73-89]

  • Hashemi Mehneh, Hamed Multidisciplinary optimization for configuration of a reentry capsule considering uncertainty [Volume 12, Issue 4, 2019, Pages 1-17]

  • Hassani, Mehdi Star Catalog Criteria Selection and Mission Catalog Update for a Typical Star Tracker [Volume 5, Issue 4, 2013, Pages 1-8]

  • Hassani, S. M. M. Fault Detection for an Aerospace Launch Vehicle Using Sliding Mode Observer [Volume 6, Issue 2, 2013, Pages 49-56]

  • Hassanpour, Halimeh Study of light spectrums effects on some growth parameters and antioxidant capacity of Anthemis gilanica [Volume 14, Issue 1, 2021, Pages 15-22]

  • Hassanpour, Halimeh Growth Mechanism of Matricaria chamomilla Plant under Space Lighting System: Induction of Pigment Synthesis, Enzyme Defense System, and Antioxidant Metabolites [Volume 16, Issue 3, 2023, Pages 69-78]

  • Heidaree, Hamid The current framework of Space Law approach to commercial space activities: prescriptive or restrictive [Volume 13, Issue 1, 2020, Pages 25-38]

  • Heidari, MohammadReza Specific Grain Analysis and Rapid Internal Ballistic Simulation for Solid Motor [Volume 5, Issue 3, 2012, Pages 67-80]

  • Heidary, M. R. Study of Hot Gas Pressurizing System Tank and Liquid Rocket Engine Interaction by Dynamic Simulation [Volume 6, Issue 1, 2013, Pages 11-19]

  • Heidary, M. R. Dynamics Simulation of Pressurizing in Propulsion System Configuration [Volume 6, Issue 3, 2013, Pages 1-13]

  • Hekmat, Azadeh Effect of Simulated Microgravity Condition on Cells Proliferation and Myostatin Gene Expression in Differentiated Skeletal Muscle Cells (C2C12) [Volume 15, Issue 2, 2022, Pages 81-92]

  • Hekmat, Azadeh The comparison of the binding parameters of silver nanoparticles to DNA in gravity and microgravity conditions [Volume 13, Issue 1, 2020, Pages 61-70]

  • Hekmati, Malek Study of light spectrums effects on some growth parameters and antioxidant capacity of Anthemis gilanica [Volume 14, Issue 1, 2021, Pages 15-22]

  • HeshmatiMoez, Alireza Design and Fabrication of a dual-polar reflector array antenna for satellite applications [Volume 13, Issue 2, 2020, Pages 99-104]

  • Heyat Davoudian, Salar Drop Behavior on Micro-Structured Superhydrophobic Coating [Volume 15, English Special Issue, 2022, Pages 25-33]

  • Heydari, Ghasem Homotopy-based optimal trajectory design to transfer from Earth orbit to halo orbits [Volume 13, Issue 3, 2020, Pages 25-38]

  • Heydari Beni, Mohsen Free Vibration Analysis of Grid Stiffened Doubly Curved Composite Shells Using a Refined Higher Order Theory [Volume 15, Issue 1, 2022, Pages 1-20]

  • Himdi, Mohamed A Reconfigurable and Steerable Horn Antenna Using Plasma Dielectric Slabs for Controllable Gain and Beam Steering [(Articles in Press)]

  • H. Korayem, M. Dynamic Modeling of Flexible Manipulators Using Finite Element Method and Optimal Control of their Motion [Volume 5, Issue 2, 2012, Pages 25-34]

  • HojatKashani, Farokh Space Application of a Linear Array of Plasma Antenna [Volume 5, Issue 3, 2012, Pages 59-66]

  • Hoseeinalipour, Seyed Mostafa Implementation of Developing Linear Hydrodynamic Instability Theory on a Hollow Cone-shaped Liquid Sheet of a Swirl Injector [Volume 11, Issue 4, 2018, Pages 1-10]

  • Hosein- Alipour, S. M. Atomyzasion Modeling the Rotating Spray Slime [Volume 4, Issue 1, 2011, Pages 39-48]

  • Hosseinalipour, S. M. Dual Base Swirl Injector Design for Increasing Specific Impluse in a Liquid-Fuel Rocket Engine [Volume 2, Issue 1, 2009, Pages 51-57]

  • Hossein Alipour, Mostafa Microscopic Test of a Swirl Injector by High-speed Photography [Volume 10, Issue 4, 2018, Pages 1-7]

  • Hosseini, A. Measurement of Neutron Irradiation Effect on Reverse Current Damage Constant α for Diode [Volume 6, Issue 2, 2013, Pages 11-19]

  • Hosseini, M.R. Investigation in to The Effect of Kinematic of The Space Craft Attitude Control Using Feedback Linearization Method [Volume 11, Issue 1, 2018, Pages 59-71]

  • Hosseini, S. A. Assessment of Solution of the Boundary Layer Equations and Approximate Relations for Aeroheating of Axisymmetric Reentry Vehicles [Volume 6, Issue 3, 2013, Pages 39-48]

  • Hosseini, S. A. Laminar and Turbulent Aero Heating Predictions over Blunt Body in Hypersonic Flow [Volume 7, Issue 1, 2014, Pages 33-40]

  • Hosseini, S. A. Automatic Reading of a Trade Gyrocompass Using Image Processing and Neural Networks [Volume 7, Issue 2, 2014, Pages 85-92]

  • Hosseini, Seyyed Majid Re-Entry Trajectory Design with Use of Aided Optimization Algorithm through Combination of Classic Guidance & Acceleration Profile Optimization [Volume 15, Issue 1, 2022, Pages 51-62]

  • Hosseini, ُshahram الگوریتم جدید فرا ابتکاری تطبیقی در تخمین وضعیت و مدل فضاپیما [Volume 12, Issue 4, 2019, Pages 79-89]

  • Hosseiniakram, Pedram Attitude Control of Nanosatellite Using Optimal Quadratic Linear and Nonlinear Methods [Volume 16, English Special Issue, 2023, Pages 51-64]

  • Hosseini Onari, Hadi HIL Experimental Analyses of Satellite Electrical Power Subsystem (EPS) in De-tumbling Mode [Volume 10, Issue 4, 2018, Pages 19-28]

  • Hosseinipanah, M. Sh. Design and Simulation of Magnetic Conductors to Enhance Features of Satellite Antennas and to Reduce Effects of Space Radiation [Volume 6, Issue 3, 2013, Pages 61-66]

  • Hosseini Sani, Seyed Kamal Nonlinear Dynamic Inversion Fault Tolerant Control for Spacecraft    [Volume 8, Issue 2, 2015, Pages 11-17]

  • HosseiniSani, S. K. Intelligent Satellite Orbit Prediction Based on Time Series Analysis [Volume 7, Issue 3, 2014, Pages 43-49]

  • Hozuri, Mansour Monopropellant Propulsion System Design using Multidisciplinary Design Optimization, Sequential Design Method, and Comparing Results [Volume 10, Issue 2, 2017, Pages 53-63]

  • Hozuri, Mansour Evaluation of Three Design approach of a bipropellant propulsion system including multidisciplinary design optimization, Robust and Optimum-Robust [Volume 12, Issue 1, 2019, Pages 41-53]

  • Hozuri, Mansour The presentation of the ARTA CanSat design and construction process at the CANSAT International Competition in Iran [Volume 13, Issue 2, 2020, Pages 63-77]

  • Hozuri, Mansour Multidisciplinary Design of Bipropellant Propulsion System in Three Methods, Optimal Design, Reliability Based Design and Optimal Reliability Based Design [Volume 14, Issue 4, 2021, Pages 85-98]

I

  • Imani, A. Robust Control of Spacecraft Formation Flying Using Optimal Sliding Mode [Volume 6, Issue 1, 2013, Pages 69-75]

  • Imani, A. Fuzzy Sliding Mode for Spacecraft Formation Control in Eccentric Orbits [Volume 7, Issue 1, 2014, Pages 49-56]

  • Irani, S. Reliability Allocation to Launch Vehicle Subsystems by Using AHP Method in Conceptual Design Phase [Volume 5, Issue 2, 2012, Pages 49-57]

  • Iranzad, M. Development of Reaction Wheel Disturbances General Model and Validation with Experimental Data [Volume 6, Issue 1, 2013, Pages 79-91]

  • Izadipour, Ahmad Comparison of Direct and Indirect Georeferencing Methods Using Satellite Linear Array Iimages [Volume 8, Issue 2, 2015, Pages 1-10]

J

  • Jafari, A. A. Effect of rotating speed and stiffeners on natural frequency of composite shell [Volume 4, Issue 1, 2011]

  • Jafari, H. Measurement of Neutron Irradiation Effect on Reverse Current Damage Constant α for Diode [Volume 6, Issue 2, 2013, Pages 11-19]

  • Jafari, H. Studying and Calculating the Radiation Damage Caused by the Solar Radiation Spectrum in the Crystal Structure of Semiconductor Components [Volume 6, Issue 3, 2013, Pages 55-60]

  • Jafari, H. Sensitive Volume Modeling in Calculation of Space Radiation-Induced SEU Cross Section [Volume 6, Issue 4, 2014, Pages 23-28]

  • Jafari, Hamid Calculation and measurement of leakage current variations due to displacement damage for a silicon diode exposed to space protons [Volume 13, Issue 4, 2020, Pages 71-79]

  • Jafari, Hamid Studying the Effects of Multi-Layer Shielding in Reducing Space Radiations Exposure of Human and Electrical Components in Space Missions [Volume 16, Issue 2, 2023, Pages 19-26]

  • Jafari, M. Space Inertial Navigation System Accuracy Increasing Using Orbit Point Mass Dynamic [Volume 6, Issue 2, 2013, Pages 57-66]

  • Jafari, Mahdi Integrated Inertial Navigation with Positioning System for Increasing Orbital Module Navigation Accuracy [Volume 5, Issue 3, 2012, Pages 11-19]

  • Jafari, Marzieh A method for determining the optimum parameter of the soft filters to image fusion in the frequency domain [Volume 14, Issue 3, 2021, Pages 23-37]

  • Jafari, Mostafa Strap-On Boosters Separation Analysis Using Coupled Simulation of Constraint Dynamics and Time Dependent CFD [Volume 15, English Special Issue, 2022, Pages 35-44]

  • Jafari -Nadoushan, M. Design of Round Trip Trajectories to Lunar L1 [Volume 6, Issue 3, 2013, Pages 49-54]

  • Jafari Nadoushan, M. Modeling Halo Orbits and the Associated Manifolds in the Restricted Three Body Problem [Volume 3, Issue 1, 2010, Pages 75-80]

  • Jafari Nadoushan, M. Studying of Effect of Regularization and Change of Independent Variable on the Solution of Perturbed 2BP [Volume 3, Issue 2, 2011, Pages 53-58]

  • Jafari Nadoushan, Mahdi Symmetric periodic solution around asteroid 216 Kleopatra and its stability in the presence of solar radiation pressure [Volume 14, Issue 1, 2021, Pages 1-13]

  • Jafari Nadoushan, Mehdi Optimal Mission Design for Moon Exploration Expedition [Volume 11, Issue 2, 2018, Pages 47-53]

  • Jafari-Nodoshan, Mahdi Economic analysis of exploitation of lunar resources [(Articles in Press)]

  • Jafarpanah, Mostafa Cost Estimation Model Presentation for Cryogenic/Semi-Crogenic Space Propulsion Systems [Volume 14, Issue 4, 2021, Pages 25-33]

  • Jafarpanah, Mostafa Cost Estimation for Space Propulsion Systems and Human Resource Cost and The Project Implementation Time Optimization [Volume 15, Issue 3, 2022, Pages 79-92]

  • Jafarsalehi, A. Satellite Conceptual Design Multi-Objective Optimization Using Co Framework [Volume 7, Issue 1, 2014, Pages 1-12]

  • Jafarsalehi, A. Comprehensive Code of Remote Sensing Satellite Conceptual Design [Volume 7, Issue 2, 2014, Pages 35-47]

  • Jafarzadeh-Khatibani, M. Positron Annihilation Spectroscopy in Materials and Technical Details of Measurement Systems [Volume 6, Issue 2, 2013, Pages 1-10]

  • Jahanbakhsh, H. Design and Fabrication of Laboratory Pilot for OSL Dosimeter System for Space Applications [Volume 6, Issue 3, 2013, Pages 67-73]

  • Jahanbakhsh, Hossein Improvement of the Electrical Potential Distribution on the Surface Geostationary Satellites using Material Change [Volume 10, Issue 3, 2017, Pages 25-39]

  • Jahangirian, A. Effects of Solar Activities, Drag Coefficient and Atmospheric Wind on Altitude Loss of a LEO Satellite [Volume 1, Issue 1, 2008, Pages 57-66]

  • Jahani, Kamal Isolation of Satellite's Sensitive Equipments from Longitudinal Vibration of Launch Vehicle Using Silicone Gel [Volume 7, Issue 4, 2015, Pages 81-91]

  • Jalali, A. Modeling of Shutdown Process in Liquid Propellant Rocket Engines [Volume 6, Issue 4, 2014, Pages 1-11]

  • Jalali Chimeh, S. A. R. Dynamic Simulation of Propellant Utilization System in Propellant Tanks of a Liquid Propellant Engine [Volume 3, Issue 2, 2011, Pages 31-43]

  • Jalali-Chimeh, S. A. R Dynamic Simulation of Flight's Apparent Velocity Regulation System [Volume 4, Issue 2, 2012, Pages 35-46]

  • Jalali Naini, Seyed Hamid Implicit Guidance Equations in Polar Coordinates [Volume 7, Issue 4, 2015, Pages 1-9]

  • Jalali Naini, Seyed Hamid Approximate Solution of Required Velocity in Elliptical Earth Model Using Piecewise Linear [Volume 9, Issue 3, 2016, Pages 1-12]

  • Jalali Naini, S. H. Approximate Solution of Sensitivity Matrix with Final Velocity Constraint Using Linear Time-Varying Gravity Assumption [Volume 4, Issue 2, 2012, Pages 71-81]

  • Jalali Naini, S. Hamid Proportional Navigation with Linear Acceleration and Line-of-Sight Acceleration Feedbacks [Volume 13, Issue 4, 2020, Pages 1-13]

  • Jalali-Naini, S. H. Closed-Loop Guidance with Final Velocity Constraint Using Time-Varying Weighting Coefficient for Shaping of Commanded Acceleration [Volume 2, Issue 3, 2009, Pages 1-12]

  • Jalali-Naini, S. H. Ascending Phase Fuzzy Logic Guidance of Satellite Launch Vehicles for Reducing the Adverse Wind Effects [Volume 7, Issue 3, 2014, Pages 75-82]

  • Jalali-Naini, S.H Robust Optimization of Satellite Attitude Control with Thruster Actuators based on Combined Objective Function [Volume 10, Issue 4, 2018, Pages 55-66]

  • Jalali-Naini, S. Hamid A Modification to Integral Pulse-Width Pulse-Frequency Modulator [Volume 14, Issue 1, 2021, Pages 55-64]

  • Jalali-Naini, S. Hamid Proportional Navigation Guidance with Variable Navigation Ratio in terms of the angle of relative velocity with respect to Line-of-Sight and its Rate [Volume 13, Issue 2, 2020, Pages 1-12]

  • Jalali-Naini, S. Hamid Miss Distance Analysis of First-Order Explicit Guidance Law with/without Radome effect [Volume 15, Issue 4, 2022, Pages 1-18]

  • Jalali-Naini, S.Hamid Static Analysis of Pulse-Width Pulse-Frequency Modulator Based on Analytical and Numerical Solutions [Volume 11, Issue 1, 2018, Pages 13-29]

  • Jaliian, Shahrokh Development of MIL and PIL testbed for Student Microsatellite Attitude Control Subsystem [Volume 13, Issue 3, 2020, Pages 51-62]

  • Jalili, Hadi Explaining the Development Strategy of Space Technology Based on the Developing Models of Countries [Volume 17, Issue 1, 2024, Pages 49-62]

  • Jalilian, Shahrokh Software Fault Tolerance Techniques for Dealing with Transient Faults in Satelite Software [Volume 5, Issue 4, 2013, Pages 9-18]

  • Jamilnia, R. Optimal Low Thrust Orbit Transfer Using Direct Collocation Method [Volume 1, Issue 2, 2008, Pages 35-42]

  • Javadi, M. M. Fabrication and Test of Flexible Joint Thrust Vector Controlling System in SRM Using Polyurethane Elastomer [Volume 5, Issue 2, 2012, Pages 75-83]

  • Javaheripour, Mahsa Design of an Nonlinear Extended State Observer to Estimate Unmeasurable Information on the Problem of Flying Objects Guidance [Volume 15, Issue 3, 2022, Pages 67-78]

  • Jodey, J. Multidisciplinary Design Optimization of a Small Launch Vehicle; a System Sensitivity Analysis Approach [Volume 1, Issue 1, 2008, Pages 47-56]

  • Jokari, Ehsan Physical Configuration Design of a 10N Monopropellant Hydrazine Thruster [Volume 12, Issue 1, 2019, Pages 13-22]

  • Joudakian, Vahid Adaptive Generalized-Minimum-Variance Attitude Control of a High Pointing-Accuracy Remote Sensing Satellite [Volume 16, English Special Issue, 2023, Pages 1-23]

K

  • Kabganian, Mansor Design and Implementation of Backstepping-Sliding mode Attitude Controller in The Prossecor in The Loop Test Bed [Volume 9, Issue 1, 2016, Pages 25-35]

  • Kahe, Ghasem A Nonlinear Attitude Controller for a Launch Abort System of a Manned Spacecraft [Volume 10, Issue 1, 2017, Pages 1-13]

  • Kahe, Ghasem Evaluation of Diversity Effects on Increasing the Reliability of Space Systems [Volume 15, English Special Issue, 2022, Pages 45-53]

  • Kahe, Ghasem Investigation of MEMS IMU Performance in Sounding Rocket [Volume 12, Issue 4, 2019, Pages 69-77]

  • Kalantari-Nezhad, R. Investigation and Analysis of Seperation System of Kavoshgar-3 [Volume 3, Issue 1, 2010, Pages 15-23]

  • Kalhor, A. Designing, Testing and Evaluation of Single Gimbal Control Moment Gyro for Microsatellite [Volume 2, Issue 1, 2009, Pages 13-23]

  • Kalhor, A. Implementation of Three Axis Attitude Controllers for Evaluation of a Micro-gravity Satellite Simulator [Volume 5, Issue 2, 2012, Pages 59-68]

  • Kalhor, A. Design, Manufacturing and Test of a Three Degrees-of-Freedom Attitude Control Simulator for an Agile Micro-Satellite Based on Single Gimbal Control Moment Gyros [Volume 7, Issue 3, 2014, Pages 51-67]

  • Kalhor, Ahmad Attitude Stability Testing of an Agile Satellite Simulator with Single-Gimbal Control-Momentum-Gyros [Volume 5, Issue 4, 2013, Pages 61-68]

  • Kalhor, Ahmad Design and Manufacturing of a Variable Speed Control Moment Gyro for an Agile Micro-Satellite Attitude Control Simulator [Volume 8, Issue 1, 2015, Pages 73-77]

  • Kalhor, Ahmad A Launch Vehicle Tracker Design Based on On-Line Linearization [Volume 9, Issue 2, 2016, Pages 1-9]

  • Kamali Moghadam, Ramin Equilibrium Effects on the Hypersonic Laminar Boundary Layer Flow over Axisymmetric Bodies [Volume 8, Issue 4, 2016, Pages 19-27]

  • Kamali Moghadam, Ramin Drop Behavior on Micro-Structured Superhydrophobic Coating [Volume 15, English Special Issue, 2022, Pages 25-33]

  • Kamali Moghadam, Ramin Design and Dynamic Analysis for Vertical and Horizontal Cylindrical Body in Reentry Flight [Volume 15, Issue 3, 2022, Pages 1-9]

  • Kamali –Moghadam, R. Assessment of Solution of the Boundary Layer Equations and Approximate Relations for Aeroheating of Axisymmetric Reentry Vehicles [Volume 6, Issue 3, 2013, Pages 39-48]

  • Kamarzarrin, Mehrnoosh Improving DGPS Accuracy Using Predictions of Reference Position Components Error Factors [Volume 8, Issue 2, 2015, Pages 41-56]

  • Kamranifar, Majid Effect of Injector Pressure Drop on The ‎Performance of A 1 N Monopropellant ‎Thruster [Volume 15, Issue 4, 2022, Pages 19-29]

  • Kamyar, R. Optimal Coupled Spacecraft Rendezvous and Docking Using Gauss Pseudospectral Method and Step by Step Linearization [Volume 2, Issue 2, 2009, Pages 1-16]

  • Karami Horestani, Ali Low-Profile Helical Antenna for Space Application [Volume 11, Issue 2, 2018, Pages 55-59]

  • Karami Horestani, Ali A Reconfigurable and Steerable Horn Antenna Using Plasma Dielectric Slabs for Controllable Gain and Beam Steering [(Articles in Press)]

  • Karami Mazraeshahi, H. Dynamic Simulation of Flight's Apparent Velocity Regulation System [Volume 4, Issue 2, 2012, Pages 35-46]

  • Karbasian, M. Modeling and Evaluation of Reliability in Rocket Engine by Fault Tree Analysis [Volume 2, Issue 2, 2009, Pages 69-73]

  • Karbasian, M. Designing an Estimation Pattern for Reliability of Launch Vehicle Structure with Bayesian Networks [Volume 5, Issue 1, 2012, Pages 73-80]

  • Karbasian, Sh. Evaluation of the Effects of Radiation, Irradiance, and Temperature on Solar Cell Electrical Characteristics and Extraction of Maximum Solar Panel Power by MPPT [Volume 1, Issue 1, 2008, Pages 67-80]

  • Karbasian, Shahab Identification and Prioritization of Satellite Electrical Power Subsystem Technologies for National Development Based on Multiple Criteria Decision Making [(Articles in Press)]

  • Kargar, A. Dual Base Swirl Injector Design for Increasing Specific Impluse in a Liquid-Fuel Rocket Engine [Volume 2, Issue 1, 2009, Pages 51-57]

  • Karim Abadeh, Moslem Spacecraft Re-entry Control using Cross and Radial Moving-Mass Actuators [(Articles in Press)]

  • Karimaei, Hadiseh Extraction of a Theoretical Energy-based Model to Estimate Mean Droplet Diameter of the Swirl Injector Spray [Volume 10, Issue 3, 2017, Pages 59-65]

  • Karimaei, Hadiseh Microscopic Test of a Swirl Injector by High-speed Photography [Volume 10, Issue 4, 2018, Pages 1-7]

  • Karimaei, Hadiseh Design and Simulation of Fuel Injector of a 10N Monopropellant Hydrazine Thruster [Volume 11, Issue 3, 2018, Pages 9-19]

  • Karimaei, Hadiseh Implementation of Developing Linear Hydrodynamic Instability Theory on a Hollow Cone-shaped Liquid Sheet of a Swirl Injector [Volume 11, Issue 4, 2018, Pages 1-10]

  • Karimaei, Hadiseh Physical Configuration Design of a 10N Monopropellant Hydrazine Thruster [Volume 12, Issue 1, 2019, Pages 13-22]

  • Karimaei, Hadiseh Provide a Predictive Model for the Preliminary Design of Swirl Injectors Based on Neuro-Fuzzy Model Thruster [Volume 12, Issue 2, 2019, Pages 11-21]

  • Karimaei, Hadiseh Design and Simulation of Single Capillary Injector and Circular Injector Plate for a Monopropellant Thruster [Volume 15, Issue 3, 2022, Pages 109-118]

  • Karimaei, Hadiseh Design and Configuration of Ground Sample Components of Low Propulsion Monopropellant Thruster Using Some Engineering Software [Volume 16, Issue 1, 2023, Pages 35-46]

  • Karimaei, Hadiseh Optimized Dimension Design of Catalytic Chamber of a 10 N Thruster [Volume 16, Issue 2, 2023, Pages 55-61]

  • Karimaghaee, Paknoosh Performance and Stability Investigation of a line of sight based Guidance System in the Presence of Measurement Noise [Volume 11, Issue 1, 2018, Pages 31-40]

  • Karimi, H. Multi-Stage Liquid Propellant Launch Vehicle Conceptual Design, Based on Combinatorial Optimization of Major Design Parameters [Volume 1, Issue 1, 2008, Pages 21-36]

  • Karimi, H. Multi-Stage Liquid Propellant Launch Vehicle Conceptual Design (LVCD) Software, Based on Multi-Parameter Optimization Idea [Volume 1, Issue 2, 2008, Pages 17-25]

  • Karimi, H. Dynamic Simulation of Propellant Utilization System in Propellant Tanks of a Liquid Propellant Engine [Volume 3, Issue 2, 2011, Pages 31-43]

  • Karimi, H. Study of Hot Gas Pressurizing System Tank and Liquid Rocket Engine Interaction by Dynamic Simulation [Volume 6, Issue 1, 2013, Pages 11-19]

  • Karimi, H. Dynamics Simulation of Pressurizing in Propulsion System Configuration [Volume 6, Issue 3, 2013, Pages 1-13]

  • Karimi, H. Modeling of Shutdown Process in Liquid Propellant Rocket Engines [Volume 6, Issue 4, 2014, Pages 1-11]

  • Karimi, Hasan Optimization of Schematic and Parameters of Staged Combustion Launch Vehicle Liquid Engines [Volume 9, Issue 1, 2016, Pages 1-11]

  • Karimi, Hasan Dynamic & Non-linear Modelling of an Expansion Cycle Rocket Engine [Volume 13, Issue 1, 2020, Pages 39-48]

  • Karimi, Nima System Design and Analysis of Launch Abort System of Manned Spacecraft in Sub-Orbital Mission [Volume 13, Issue 1, 2020, Pages 13-23]

  • Karimian, Seyed Mohammad Hossein Evaluation of Effective Emissivity of a Multilayer Insulation Blanket Using Test [Volume 8, Issue 1, 2015, Pages 19-25]

  • Karimian, S.M.Hossein Analysis of the Effect of Layer Perforation Pattern on the Rate of Gas Leakage from Multilayer Thermal Insulation During Satellite Launch [Volume 16, Issue 1, 2023, Pages 11-21]

  • Karimzadeh Baee, Roghieh Investigating the Test and Evaluation of GaN Transistors Radiation Resistance in SSPA Amplifier Board in LEO Satellite Payload [Volume 16, Issue 1, 2023, Pages 59-74]

  • Karimzadeh Baee, Roghieh A Review of the Applications of Artificial Intelligence in Improving the Performance of Integrated Space-Air and Ground Networks [Volume 16, Issue 2, 2023, Pages 27-42]

  • Karimzadeh Baee, Roghieh Determining Allowed Positions of Aeronautical-Earth Station in Motion (A-ESIM) Prevent its Frequency Interference in the Fixed Ground Station [Volume 16, Issue 3, 2023, Pages 1-14]

  • Kasaeian, Seyed Aliakbar Dynamic Terminal Sliding Mode Control for an Aerospace Launch Vehicle [Volume 8, Issue 4, 2016, Pages 1-7]

  • Kashani, H. Analysis of Random Positioning System for Simulation of Microgravity [Volume 2, Issue 1, 2009, Pages 25-34]

  • Kashani, Hamed Impulsive Load Destructive Effects Reduction in Launch Vehicles Using Structural Joint [Volume 16, Issue 3, 2023, Pages 27-36]

  • Kashaninia, Abdol Reza Design a μ-Controller ToControl Attitude of a Flexible Microsatellite [Volume 8, Issue 1, 2015, Pages 61-71]

  • Kasiri, Ali Adaptive Generalized-Minimum-Variance Attitude Control of a High Pointing-Accuracy Remote Sensing Satellite [Volume 16, English Special Issue, 2023, Pages 1-23]

  • Kaviri, Samane Design and implementation of hardware-in-the-loop (HIL) test-bed for spacecraft attitude control [Volume 12, Issue 2, 2019, Pages 55-70]

  • KavoshTehrani, M. Automatic Reading of a Trade Gyrocompass Using Image Processing and Neural Networks [Volume 7, Issue 2, 2014, Pages 85-92]

  • Kazemi, Ali The Effects of Simulated Microgravity on Serum Levels of VEGF in Male Wistar Rats [Volume 9, Issue 4, 2017, Pages 63-68]

  • Kazemi, Ali Title: Effect of six-week high intensity interval training under simulated microgravity condition on morphology of radial nerve myelin sheet in male rats [Volume 12, Issue 2, 2019, Pages 71-78]

  • Kazemi, H. Process of Liability Principles in International Space Law [Volume 5, Issue 2, 2012, Pages 35-48]

  • Kazemi, H. Passage of Space Objects over the Territory of States from the Perspective of the International Law [Volume 7, Issue 3, 2014, Pages 33-42]

  • Kazemi, H. Role of States in Regulating Space Activities in International Law [Volume 9, Issue 4, 2017, Pages 27-37]

  • Kazemi, Hamid Legal Aspects of the mining of celestial bodies and its challenges [Volume 11, Issue 4, 2018, Pages 51-64]

  • Kazemi, Hamid States' Responsibility to Operate Small Satellites in International Space Law [Volume 14, Issue 2, 2021, Pages 89-102]

  • Kazemi, Hamid Collision Prediction of Spacecraft for Space Traffic Management [Volume 15, Issue 2, 2022, Pages 93-102]

  • Kazemi, Hamid The Intellectual Property Rights and Transfer of Technology in Space Industry [Volume 15, Issue 1, 2022, Pages 107-119]

  • Kazemi Hokmabad, Aida Study of Space Weather and its Risks on Human Biologic Processes [Volume 16, Issue 3, 2023, Pages 51-68]

  • Kazerooni, Hanif Presentation of a conceptual framework for the design of Chabahar strategic launch site for the development of Iran space industry [Volume 13, Issue 1, 2020, Pages 83-98]

  • Keshtegar, Behrooz Maximum Likelihood-Based Worst-Case Optimization Design of Hydrazine Propulsion System for aSatellite Orbital Transfer System under Uncertainty [Volume 14, Issue 3, 2021, Pages 1-14]

  • Khadivi, Azade Dimensional Direct Simulation Monte Carlo Simulation of Thruster Plumes [Volume 15, Issue 2, 2022, Pages 43-58]

  • Khaghani, M. Positron Annihilation Spectroscopy in Materials and Technical Details of Measurement Systems [Volume 6, Issue 2, 2013, Pages 1-10]

  • Khaladjzadeh, L. Drivation of System Level Characteristics of a Manned Spacecraft by Applying Statistics Models [Volume 3, Issue 1, 2010, Pages 25-36]

  • Khalaj AmirHoseini, Mohamad Design and Fabrication of a dual-polar reflector array antenna for satellite applications [Volume 13, Issue 2, 2020, Pages 99-104]

  • Khalaj-Zade, L.. Conceptual Design Algorithm of Dousti Manned Spacecraft [Volume 4, Issue 2, 2012, Pages 11-22]

  • Khaledi, Neda The Effects of Simulated Microgravity on Serum Levels of VEGF in Male Wistar Rats [Volume 9, Issue 4, 2017, Pages 63-68]

  • Khani Chamani, Masoome Economic analysis of exploitation of lunar resources [(Articles in Press)]

  • Khankalantary, Saeed Optimal Proportional Navigation in Three-Dimensional Space Using Model Predictive Control Approach [Volume 14, Issue 4, 2021, Pages 51-59]

  • Khatoon Abadi Kalali, Seyede Elahe Study of Space Weather and its Risks on Human Biologic Processes [Volume 16, Issue 3, 2023, Pages 51-68]

  • Kheirdoost, Ali Scientometric analysis of published scientific productions in the field of satellite constellations [(Articles in Press)]

  • Kheirkhah, Sajjad The presentation of the ARTA CanSat design and construction process at the CANSAT International Competition in Iran [Volume 13, Issue 2, 2020, Pages 63-77]

  • Khodabandeh, Amir Kinematic Standard Point Positioning (SPP) based on Kalman Filter and C/A Code Observations Under Intense Geomagnetic Storm Conditions [Volume 14, Issue 3, 2021, Pages 101-108]

  • Khodadadiyan, S. Neural Network Based Diagnostic Indication of a Liquid Propellant Engine with Faulty Data Collection System [Volume 7, Issue 2, 2014, Pages 75-83]

  • Khodadadiyan, Sajad Optimization of Schematic and Parameters of Staged Combustion Launch Vehicle Liquid Engines [Volume 9, Issue 1, 2016, Pages 1-11]

  • Khoshsima, Masoud Modeling and calculating the albedo and IR heat flux applied to satellite based on the geographic position of sarellite [Volume 11, Issue 4, 2018, Pages 23-30]

  • Khoshsima, Masoud Study of Modeling Parameters in Determination of TID, DD, and SEE Radiation Damages for Satellite in LEO Orbit Using OMERE Software [Volume 12, Issue 3, 2019, Pages 63-71]

  • Khoshsima, Masoud Rapid Performance Sizing of Reaction Wheels in a Very High Resolution Remote Sensing Satellite Using Matching Diagram Technique [Volume 15, Issue 1, 2022, Pages 21-39]

  • Khoshsima, Masoud Design and sensitivity analysis of an Earth observation mission's operating orbit in the absence of injection into the Sun-synchronous orbit [Volume 14, Issue 4, 2021, Pages 1-9]

  • Khoshsima, Masoud Thermal Modeling of Lidar Payload in a Remote Sensing Satellite under System Level Considerations with a Review on its Challenges [Volume 16, Issue 2, 2023, Pages 79-91]

  • Khoshsima, Masoud Economic analysis of exploitation of lunar resources [(Articles in Press)]

  • Khosravi, Mehrdad Multi objective design optimization of heat pipes configuration attached to the solar panels of a sun pointing satellite [Volume 12, Issue 1, 2019, Pages 55-68]

  • Khosrobeygi, Hamed Investigation of a Bi-propellant Thruster by a Developed Space Engine’s Thrust Chamber Analysis Code [Volume 14, Issue 2, 2021, Pages 47-37]

  • Kiani, Maryam Optimal Multiple-Impulse Orbit Transfer Utilizing Pseudo-Newton Method [Volume 11, Issue 1, 2018, Pages 49-57]

  • Kiani, Maryam Investigation of the conduction effect on temperature-based attitude estimation [Volume 12, Issue 4, 2019, Pages 91-102]

  • Kiani, Maryam Homotopy-based optimal trajectory design to transfer from Earth orbit to halo orbits [Volume 13, Issue 3, 2020, Pages 25-38]

  • Kochaki, Jafar Introduction to Tadbir satellite Orbit Determination System [Volume 8, Issue 3, 2015, Pages 65-70]

  • Kohandani, Reza Free Vibration Analysis of Grid Stiffened Doubly Curved Composite Shells Using a Refined Higher Order Theory [Volume 15, Issue 1, 2022, Pages 1-20]

  • Koolivand, Yarollah Designing and Evaluation of an Experimental Attitude Determination System Using Sun Sensor and Magnetometer [Volume 5, Issue 4, 2013, Pages 69-78]

  • Kosari, Amirreza A Launch Vehicle Tracker Design Based on On-Line Linearization [Volume 9, Issue 2, 2016, Pages 1-9]

  • Kosari, Amirreza Design and sensitivity analysis of an Earth observation mission's operating orbit in the absence of injection into the Sun-synchronous orbit [Volume 14, Issue 4, 2021, Pages 1-9]

  • Kosari, Amir Reza Satellite 3Axis Attitude Control Using the Combination of Reaction Wheels and Thrusters [Volume 11, Issue 3, 2018, Pages 63-71]

  • Kosari, Amir Reza Rapid Performance Sizing of Reaction Wheels in a Very High Resolution Remote Sensing Satellite Using Matching Diagram Technique [Volume 15, Issue 1, 2022, Pages 21-39]

  • Kosari, Amir Reza Study of Space Weather and its Risks on Human Biologic Processes [Volume 16, Issue 3, 2023, Pages 51-68]

  • Kosari, AmirReza Determine the Optimal Orbit for an Earth Observation Satellite Considering the Power [Volume 9, Issue 3, 2016, Pages 27-36]

  • Kosari, A. R. Hybrid Estimation of Gyro Model Parameters and GEO Satellite Moment of Inertia with Extended Kalman Filter [Volume 6, Issue 2, 2013, Pages 67-74]

  • Kosari, Ehsan Study of Space Weather and its Risks on Human Biologic Processes [Volume 16, Issue 3, 2023, Pages 51-68]

  • Kosari, Ehsan Identification and Prioritization of Satellite Electrical Power Subsystem Technologies for National Development Based on Multiple Criteria Decision Making [(Articles in Press)]

L

  • Labibian, Amir Investigation of the conduction effect on temperature-based attitude estimation [Volume 12, Issue 4, 2019, Pages 91-102]

  • Labibian, Amir Development of an EKF Based Gyro Calibration Method for High-Precision Attitude Estimation [Volume 17, Issue 1, 2024, Pages 11-20]

  • Lashkanpour, Majed Effect of Time Separation between Observations on Angles-only Preliminary Orbit Determination [Volume 8, Issue 2, 2015, Pages 19-26]

M

  • Maani, Ehsan GEO satellite station keeping mass design based on data mining [Volume 14, Issue 1, 2021, Pages 23-33]

  • Madadkar, Abdollah A Launch Vehicle Tracker Design Based on On-Line Linearization [Volume 9, Issue 2, 2016, Pages 1-9]

  • Maghsoudi Mehrabani, M. Effect of rotating speed and stiffeners on natural frequency of composite shell [Volume 4, Issue 1, 2011]

  • Mahdavi, Mahsa Structural Design Modification of a CubeSat Regarding Modal Compatibility for Launching by Vega C Launcher [Volume 16, Issue 4, 2023, Pages 41-56]

  • Mahdavy Moghaddam, H. Fabrication and Test of Flexible Joint Thrust Vector Controlling System in SRM Using Polyurethane Elastomer [Volume 5, Issue 2, 2012, Pages 75-83]

  • Mahdavy-Moghaddam, Hossein 2D Simulation of Designed Dual Throat Nozzle using Geometrical Analogy [Volume 10, Issue 2, 2017, Pages 23-32]

  • Mahdavy-Moghaddam, Hossein Simulation and Parametric Analysis of Thrust Reverser System in Solid Fuel Engines [Volume 16, Issue 2, 2023, Pages 1-17]

  • Mahmoodzadeh Entezari, Seyed Moein Thermal Optimum Trajectory Design of Manned Reentry Vehicles using the Aerodynamic Database Management Method [Volume 13, Issue 2, 2020, Pages 51-61]

  • Mahmoud-Aghdami, Ashkan Design and Fabrication of Spool Type Pin Puller Mechanism- from Concept to Qualification Model [Volume 9, Issue 3, 2016, Pages 37-51]

  • Mahmoudi, s. Hadi The current framework of Space Law approach to commercial space activities: prescriptive or restrictive [Volume 13, Issue 1, 2020, Pages 25-38]

  • Mahmoudian, Seyed Mohammadreza Design, Fabrication, and Test of a Cryogenic Liquid Oxygen-Ethanol Engine [Volume 16, Issue 1, 2023, Pages 47-58]

  • Mahmoudkhani, Saeed Parametric Study of Aeroelastic Instability Boundaries of Space Launch Vehicle in Subsonic Flow [Volume 15, Issue 3, 2022, Pages 49-66]

  • Makhdoum, M. F. Remote Sensing Role in Land Use StudiesCase Study: Tehran Metropolitan and its Boundary [Volume 7, Issue 3, 2014, Pages 69-73]

  • Malekan, M. A New Approach to Design an Optimum Launch Window for a Sample Micro-Satellite [Volume 6, Issue 4, 2014, Pages 43-52]

  • Maleki, Abolfazl Effect of Time Separation between Observations on Angles-only Preliminary Orbit Determination [Volume 8, Issue 2, 2015, Pages 19-26]

  • Maleki, Hamid A New Approach to Engineering Change Management for Spce Projects [Volume 14, Issue 1, 2021, Pages 43-54]

  • Malekie, Shahryar Experimental Study of the Effect of Using Space Sandwich Structures for Protection Against Space Radiation [Volume 15, Issue 2, 2022, Pages 59-69]

  • Malekpour, F. Satellite Status Control Using Tabulation Gain Controller in a Variable Parameter System [Volume 15, Issue 2, 2022, Pages 15-25]

  • Mansori-Nezhad, Hosein Identification of Space Deployable Mechanisms [Volume 9, Issue 3, 2016, Pages 53-71]

  • Mansour Fallah, Tania Efficiency of the least squares support vector regression in local modeling of the ionosphere total electron content and comparison with other models [Volume 17, Issue 1, 2024, Pages 21-36]

  • Marzban, Sh. A Method for Performance Enhancement for Aeronautical Telemetry Radio Link Using Alamouti Code [Volume 3, Issue 2, 2011, Pages 1-9]

  • Marzban, SH. Designing and Simulating the Aeronautical Telemetry Radio Link for an Air Vehicle with Fast Maneuver [Volume 2, Issue 1, 2009, Pages 1-12]

  • Marzban, Shahrokh Improvement of Bit Error Rate (BER) in Telemetry Radio Link of Satellite LEO Using MIMO Technique [Volume 5, Issue 3, 2012, Pages 21-31]

  • Mashhadi, Khashayar The presentation of the ARTA CanSat design and construction process at the CANSAT International Competition in Iran [Volume 13, Issue 2, 2020, Pages 63-77]

  • Masnadi-Shirazi, Mohamad Ali SAR Ground Moving Target Imaging based on Sparse Representation [Volume 14, Issue 3, 2021, Pages 91-100]

  • Mazaheri, Karim Effects of Geometrical Parameters of Gas Flow Channels on Polymer Electrolyte Membrane Fuel Cell Performance [Volume 15, English Special Issue, 2022, Pages 1-13]

  • Mehdi-Abadi, Mehran Satellite Spin Stabilization by Magnetic Torquers and Validation with Air-Bearing Simulator [Volume 9, Issue 2, 2016, Pages 25-34]

  • Mehmandoost-Khajeh-Dad, A. A. Positron Annihilation Spectroscopy in Materials and Technical Details of Measurement Systems [Volume 6, Issue 2, 2013, Pages 1-10]

  • Mehrabi, Ali Satellite Adaptive Attitude Control Based on Decentralized Minimal Control in the Presence of Reaction wheel Accurate Model [Volume 9, Issue 1, 2016, Pages 59-72]

  • Mehrafrooz, Mijtaba Investigation of MEMS IMU Performance in Sounding Rocket [Volume 12, Issue 4, 2019, Pages 69-77]

  • Mehrafroz, Z. A Reliability Growth Model for a Launch Vehicle With its Requirements [Volume 2, Issue 1, 2009, Pages 35-42]

  • Meshkani, R. Study of Recovery System Performance of a Sounding Rocket using Launching Tests [Volume 7, Issue 2, 2014, Pages 23-33]

  • M. Gheitaghy, A. Satellite Thermal Modeling and Analysis with the Electrical Network Method [Volume 5, Issue 1, 2012, Pages 81-90]

  • M. Hossainali, M. 3D Modeling of Ionospheric Tomography Using GPS Observations Geodynamics Network of Iran in Three Different Seasons [Volume 4, Issue 1, 2011, Pages 1-14]

  • Mikaniki, Pouria Effect of Injector Pressure Drop on The ‎Performance of A 1 N Monopropellant ‎Thruster [Volume 15, Issue 4, 2022, Pages 19-29]

  • Mikaniki, Pouria Design, Fabrication, and Test of a Cryogenic Liquid Oxygen-Ethanol Engine [Volume 16, Issue 1, 2023, Pages 47-58]

  • Miller, Reinhard Drop Behavior on Micro-Structured Superhydrophobic Coating [Volume 15, English Special Issue, 2022, Pages 25-33]

  • Miri Roknabadi, S. H. Spacecraft Optimal Attitude Control by means of Reaction Wheels [Volume 2, Issue 3, 2009, Pages 35-42]

  • Miri Roknabadi, S.H. Design and Manufacturing Steps of a Satellite Reaction Wheel [Volume 2, Issue 2, 2009, Pages 61-68]

  • Mirsajedi, S. M. Effects of Erosive Burning on Solid Rocket Motor Internal Ballistics [Volume 5, Issue 2, 2012, Pages 69-74]

  • Mirsajedi, S. M. Second Order Level Set Method in Numerical Simulation of the Grain Burn-Back [Volume 7, Issue 3, 2014, Pages 23-32]

  • Mirshams, M. Multi-Stage Liquid Propellant Launch Vehicle Conceptual Design, Based on Combinatorial Optimization of Major Design Parameters [Volume 1, Issue 1, 2008, Pages 21-36]

  • Mirshams, M. Multi-Stage Liquid Propellant Launch Vehicle Conceptual Design (LVCD) Software, Based on Multi-Parameter Optimization Idea [Volume 1, Issue 2, 2008, Pages 17-25]

  • Mirshams, M. Constrained Optimization of Launch Vehicle Trajectory Using Spline and Bezier Curves [Volume 2, Issue 2, 2009, Pages 51-60]

  • Mirshams, M. Design and Manufacturing Steps of a Satellite Reaction Wheel [Volume 2, Issue 2, 2009, Pages 61-68]

  • Mirshams, M. Drivation of System Level Characteristics of a Manned Spacecraft by Applying Statistics Models [Volume 3, Issue 1, 2010, Pages 25-36]

  • Mirshams, M. Conceptual Design Algorithm of Dousti Manned Spacecraft [Volume 4, Issue 2, 2012, Pages 11-22]

  • Mirshams, M. Reliability Allocation to Launch Vehicle Subsystems by Using AHP Method in Conceptual Design Phase [Volume 5, Issue 2, 2012, Pages 49-57]

  • Mirshams, M. Satellite Conceptual Design Multi-Objective Optimization Using Co Framework [Volume 7, Issue 1, 2014, Pages 1-12]

  • Mirshams, M. Comprehensive Code of Remote Sensing Satellite Conceptual Design [Volume 7, Issue 2, 2014, Pages 35-47]

  • Mirshams, M. Comprehensive Pattern in Designing Low-Thrust Space Propulsion Systems [Volume 7, Issue 3, 2014, Pages 9-21]

  • Mirshams, M. Optimal Control of a Tri-axial Spacecraft Simulator Test bed Actuated by Reaction Wheels [Volume 8, Issue 4, 2016, Pages 35-44]

  • Mirshams, Mehran Launch Vehicle Classical Design Software with Training Approach in Higher Education [Volume 9, Issue 3, 2016, Pages 73-79]

  • Mirshams, Mehran A Software for Establishing Technical Specifications of GEO Communication Satellites [Volume 10, Issue 3, 2017, Pages 1-14]

  • Mirshams, Mehran GEO Communication Satellite Engineering Design Code [Volume 10, Issue 4, 2018, Pages 41-54]

  • Mirshams, Mehran Optimal Mission Design for Moon Exploration Expedition [Volume 11, Issue 2, 2018, Pages 47-53]

  • Mirshams, Mehran Development of MIL and PIL testbed for Student Microsatellite Attitude Control Subsystem [Volume 13, Issue 3, 2020, Pages 51-62]

  • Mirshams, Mehran Design and Implementation of a Balance System for the CubeSat Attitude Determination and Control Tabletop Simulator [Volume 16, Issue 1, 2023, Pages 75-88]

  • Mirshams, Mehrn Complementary Method the Conceptual Design of Space Craft Electrical Power  Subsystem [Volume 8, Issue 3, 2015, Pages 55-63]

  • Mirshams, S. M. Spacecraft Optimal Attitude Control by means of Reaction Wheels [Volume 2, Issue 3, 2009, Pages 35-42]

  • Mir Shams, Mehran Inertial navigation position error estimation, using vision system [Volume 14, Issue 3, 2021, Pages 75-90]

  • Mirzaei, Amirhossein Miss Distance Analysis of First-Order Explicit Guidance Law with/without Radome effect [Volume 15, Issue 4, 2022, Pages 1-18]

  • Mirzaei, H.R. Attitude Control of Spacecraft by State Dependent Riccati Equation and Power Series Expansion of Riccati Methods [Volume 7, Issue 4, 2015, Pages 39-49]

  • Mirza Kuchaki, Satar Precise Positioning in GPS Receivers for Very High Velocities Using Combination of Recursive Least Squares and Fuzzy Logic [Volume 7, Issue 4, 2015, Pages 63-72]

  • M. Moghaddam, M Satellite Attitude Control by Magnetic Torquers with Variable Magnetic Intensity for Optimization of Power Consumption [Volume 1, Issue 1, 2008, Pages 37-45]

  • Moallem, P. Automatic Reading of a Trade Gyrocompass Using Image Processing and Neural Networks [Volume 7, Issue 2, 2014, Pages 85-92]

  • Moeini, Esmaiel Evaluation of Effective Emissivity of a Multilayer Insulation Blanket Using Test [Volume 8, Issue 1, 2015, Pages 19-25]

  • Moeini, Hamed Effects of Geometrical Parameters of Gas Flow Channels on Polymer Electrolyte Membrane Fuel Cell Performance [Volume 15, English Special Issue, 2022, Pages 1-13]

  • Moezzi, S. Andishe SAR Ground Moving Target Imaging based on Sparse Representation [Volume 14, Issue 3, 2021, Pages 91-100]

  • Mofakham Naser Eslami, Negar Military Use and Arms Race in Space from the Perspective of International Law [Volume 15, Issue 4, 2022, Pages 57-70]

  • Moghadas Najaf Abad, Hamid Reza A New Approach to Engineering Change Management for Spce Projects [Volume 14, Issue 1, 2021, Pages 43-54]

  • Moghanipoor, Marjan Investigation of the conduction effect on temperature-based attitude estimation [Volume 12, Issue 4, 2019, Pages 91-102]

  • Mohamadi, Leila Investigation and feasibility study of using components with different categories from the perspective of radiation damage in LEO and GEO orbits [Volume 14, Issue 4, 2021, Pages 11-23]

  • Mohamadi, Peiman Design, Simulation, Fabrication and Determining the Equivalent Circuit Model of a Reconfigurable FSS unit Cell Filter for Electromagnetic Protection of Space Payload Systems [Volume 16, Issue 4, 2023, Pages 71-82]

  • Mohamedpour, K. Designing and Simulating the Aeronautical Telemetry Radio Link for an Air Vehicle with Fast Maneuver [Volume 2, Issue 1, 2009, Pages 1-12]

  • Mohamedpour, Kamal Improvement of Bit Error Rate (BER) in Telemetry Radio Link of Satellite LEO Using MIMO Technique [Volume 5, Issue 3, 2012, Pages 21-31]

  • Mohamed-Pour, K. A Method for Performance Enhancement for Aeronautical Telemetry Radio Link Using Alamouti Code [Volume 3, Issue 2, 2011, Pages 1-9]

  • Mohammadi, A. Required Velocity Calculation in the Presence Of Atmosphere Effect in C* Matrix [Volume 4, Issue 1, 2011, Pages 69-78]

  • Mohammadi, Ali A New Backstepping Sliding Mode Guidance Law Considering Control Loop Dynamics [Volume 8, Issue 4, 2016, Pages 9-17]

  • Mohammadi, Alireza Numerical study on spray characteristic of double phases internal mix atomizer with Lagrangian approach [Volume 13, Issue 4, 2020, Pages 15-23]

  • Mohammadi, Karim SEU Rate and Reliability Analysis in LEO Satellites [Volume 5, Issue 3, 2012, Pages 1-9]

  • Mohammadi, Leila A Review of the Applications of Artificial Intelligence in Improving the Performance of Integrated Space-Air and Ground Networks [Volume 16, Issue 2, 2023, Pages 27-42]

  • Mohammadi, Leila Gap Analysis in Satellite Communication Services [Volume 16, Issue 4, 2023, Pages 29-40]

  • Mohammadi, Leyla Atmospheric Doppler Modelling for Open Loop Tracking in GPS-RO Receivers [Volume 9, Issue 2, 2016, Pages 35-46]

  • Mohammadi, M. S. A New Approach to Design an Optimum Launch Window for a Sample Micro-Satellite [Volume 6, Issue 4, 2014, Pages 43-52]

  • Mohammadi, Peyman Increasing the Efficiency and Reliability of the High-Power Supply With the Application of TWTA Lamps [Volume 17, Issue 1, 2024, Pages 37-48]

  • Mohammadi, Reza Evaluation of Changes in the Expression Level of some Genes Involved in Decompression Sickness in the Pressure Changes [Volume 15, Issue 1, 2022, Pages 41-49]

  • Mohammadi Amin, Meysam Parametric Study of Aeroelastic Instability Boundaries of Space Launch Vehicle in Subsonic Flow [Volume 15, Issue 3, 2022, Pages 49-66]

  • Mohammadi Amin, Meysam Thermal Optimum Trajectory Design of Manned Reentry Vehicles using the Aerodynamic Database Management Method [Volume 13, Issue 2, 2020, Pages 51-61]

  • Mohammadi-Amin, Maysam A Nonlinear Attitude Controller for a Launch Abort System of a Manned Spacecraft [Volume 10, Issue 1, 2017, Pages 1-13]

  • Mohammadkhani, Gholamreza Atmospheric Doppler Modelling for Open Loop Tracking in GPS-RO Receivers [Volume 9, Issue 2, 2016, Pages 35-46]

  • Mohammadzadeh, N. Alterations in Blood Cells Due to Increased Exposure in Space [Volume 6, Issue 2, 2013, Pages 43-48]

  • Mohammadzaman, E. Short Time Stability Approach to Guidance Law Design [Volume 3, Issue 1, 2010, Pages 37-44]

  • Mohammadzaman, Iman Integrated Guidance and Control Design by Combining Backstepping and Sliding Mode Control Methods [Volume 9, Issue 4, 2017, Pages 39-50]

  • Mohasel afshari, Behzad Modeling and calculating the albedo and IR heat flux applied to satellite based on the geographic position of sarellite [Volume 11, Issue 4, 2018, Pages 23-30]

  • Mohsenipour, Reza Design a μ-Controller ToControl Attitude of a Flexible Microsatellite [Volume 8, Issue 1, 2015, Pages 61-71]

  • Mokhtari, Majid Experimental Study of the Effect of Using Space Sandwich Structures for Protection Against Space Radiation [Volume 15, Issue 2, 2022, Pages 59-69]

  • Momeni, H. R. Short Time Stability Approach to Guidance Law Design [Volume 3, Issue 1, 2010, Pages 37-44]

  • Momeni, Morad Designing and Evaluation of an Experimental Attitude Determination System Using Sun Sensor and Magnetometer [Volume 5, Issue 4, 2013, Pages 69-78]

  • Momeni rad, Ahmad Military Use and Arms Race in Space from the Perspective of International Law [Volume 15, Issue 4, 2022, Pages 57-70]

  • Moosavi, F. Developing Attitude Control for Suborbital Module Based on Cold Gas Thrusters and Using Quaternion Feedback [Volume 6, Issue 1, 2013, Pages 1-10]

  • Moosavi, Seyed Hossein Effective Parameters of the Aluminum Particles Cyclone Separator in the Effervescent Fuel [Volume 10, Issue 1, 2017, Pages 35-45]

  • Moosavi, Seyed Hossein Prediction of droplet size and velocity distribution based on maximum entropy formulation by nonlinear instability analysis of liquid sheet spray and turbulent of nozzle flow [Volume 13, Issue 1, 2020, Pages 1-11]

  • Moradi, Masoud Improvement of the forest canopy density model based on the addition of the FCC index and the average kernel implementation [Volume 14, Issue 2, 2021, Pages 27-36]

  • Moradi, R. Optimal Coupled Spacecraft Rendezvous and Docking Using Gauss Pseudospectral Method and Step by Step Linearization [Volume 2, Issue 2, 2009, Pages 1-16]

  • Moradi, Samad Dynamic and Stability Analysis of a Cracked Rotating Flexible Beam [Volume 14, Issue 3, 2021, Pages 51-63]

  • Moradi, Samad Active Vibration Control of a Maneuvering Flexible Spacecraft Using Hybrid Actuators: A Lyapunov-Based Control Approach [Volume 15, Issue 2, 2022, Pages 1-13]

  • Moradi, Samad Form-Finding and Free Vibration Analysis of a Class-One Triplex Tensegrity Prism [Volume 16, Issue 3, 2023, Pages 15-26]

  • Mortazavi, M. هدایت بهینه بر خط بازگشت به زمین از طریق بسط مجانبی هماهنگ [Volume 3, Issue 2, 2011, Pages 69-76]

  • Mortazavi, M. A New Approach to Design an Optimum Launch Window for a Sample Micro-Satellite [Volume 6, Issue 4, 2014, Pages 43-52]

  • Mortazavi, Mahdi Model-Free Predictive Fault-Tolerant Control for Spacecraft Roto-Translational Relative Motion [Volume 14, Issue 1, 2021, Pages 77-92]

  • Mortazavi, Mehdi Design, Construction, Test and Modeling of Triaxial Helmholtz Coil for Magnetic Tests of Satellite [Volume 9, Issue 2, 2016, Pages 11-24]

  • Mortazavi, Mohammad Reza Optimal Control of a Flexible Spacecraft in a Proximity Operation Using State Dependent Riccati Equation Approach [Volume 8, Issue 1, 2015, Pages 27-41]

  • Mortazavi, Seyed Hossein Analytical Solution to Relative Motion Dynamics in Satellite Formation Flying Using Geostationary Orbit Sets [Volume 7, Issue 4, 2015, Pages 11-21]

  • Mortazavi-Bek, Mehdi Satellite Adaptive Attitude Control Based on Decentralized Minimal Control in the Presence of Reaction wheel Accurate Model [Volume 9, Issue 1, 2016, Pages 47-56]

  • Mosallaei, Nilofar Heterologous Expression of Shiga-Like Toxin Type 2 in Microgravity Condition [Volume 15, Issue 4, 2022, Pages 97-106]

  • Mosavi, Seyed Mohammad Reza Precise Positioning in GPS Receivers for Very High Velocities Using Combination of Recursive Least Squares and Fuzzy Logic [Volume 7, Issue 4, 2015, Pages 63-72]

  • Mosavi Mashhadi, Seyed Kamaleddin (Technical Note) Design and Construction of Star Tracker Platform in Order to Satellite Attitude Determination Based on Star Tracking Algorithm [Volume 9, Issue 2, 2016, Pages 85-90]

  • Mosayebi,, Armin Experimental Study of the Effect of Using Space Sandwich Structures for Protection Against Space Radiation [Volume 15, Issue 2, 2022, Pages 59-69]

  • Moslehi, Amir Determination of the Sensitive Volume and Critical Charge for Induction of SEU in Nanometer SRAMs [Volume 16, Issue 2, 2023, Pages 43-54]

  • Mossavi, A. Design and Fabrication of Laboratory Pilot for OSL Dosimeter System for Space Applications [Volume 6, Issue 3, 2013, Pages 67-73]

  • Mosvi, Seyed Mohammad Sadegh Design, Construction, Test and Modeling of Triaxial Helmholtz Coil for Magnetic Tests of Satellite [Volume 9, Issue 2, 2016, Pages 11-24]

  • Moumivand, Mohammad Investigating the Effective Numerical Solution Parameters in Calculating the Roll Damping Coefficient [Volume 10, Issue 2, 2017, Pages 65-72]

  • Mousavi, Fateme The Effect of Extreme Temperature Fluctuations Simulated of Space on the Electrophoretic Profile of Tomato (Lycopersicum esculentum Mill.) Seed Storage Proteins [Volume 16, Issue 4, 2023, Pages 83-89]

  • Mousavi, Fateme Plant Germplasm and Extreme Conditions of Outer Space [Volume 16, English Special Issue, 2023, Pages 65-71]

  • Mousazadeh, K. SAR Imaging Systems Performance Modeling [Volume 6, Issue 1, 2013, Pages 47-56]

  • Mousivand, Ehsan Identification and Prioritization of Satellite Electrical Power Subsystem Technologies for National Development Based on Multiple Criteria Decision Making [(Articles in Press)]

  • Movafeghi, A. Alterations in Blood Cells Due to Increased Exposure in Space [Volume 6, Issue 2, 2013, Pages 43-48]

  • Movahednejad, Ehsan Microscopic Test of a Swirl Injector by High-speed Photography [Volume 10, Issue 4, 2018, Pages 1-7]

  • Movahed-Nezhad, E. Atomyzasion Modeling the Rotating Spray Slime [Volume 4, Issue 1, 2011, Pages 39-48]

  • Mozafari, A. Effect of rotating speed and stiffeners on natural frequency of composite shell [Volume 4, Issue 1, 2011]

N

  • Nadafi – Pour Meibody, Mohammad Design, Manufacture and Experimental Study of a Hydrogen Peroxide-HTPB Hybrid Rocket Motor [Volume 5, Issue 4, 2013, Pages 19-28]

  • Naderi, M. Modeling of Shutdown Process in Liquid Propellant Rocket Engines [Volume 6, Issue 4, 2014, Pages 1-11]

  • Naderifar, Javad Launch Vehicle Classical Design Software with Training Approach in Higher Education [Volume 9, Issue 3, 2016, Pages 73-79]

  • Naderi Tabrizi, M. Dynamic Simulation of Propellant Utilization System in Propellant Tanks of a Liquid Propellant Engine [Volume 3, Issue 2, 2011, Pages 31-43]

  • Naderi-Tabrizi, M. Dynamic Simulation of Flight's Apparent Velocity Regulation System [Volume 4, Issue 2, 2012, Pages 35-46]

  • Nadi, M. Analysis of Navid Satellite TLE Data and it’s Effects on Tracking Operations by the Ground Stations [Volume 6, Issue 2, 2013, Pages 29-42]

  • Nadjafi, Mohammad FMECA-Based Risk Assessment in Monopropellant Hydrazine Propulsion System [Volume 16, English Special Issue, 2023, Pages 39-50]

  • Naghash, A. Effects of Solar Activities, Drag Coefficient and Atmospheric Wind on Altitude Loss of a LEO Satellite [Volume 1, Issue 1, 2008, Pages 57-66]

  • Naghash, A. Optimal Low Thrust Orbit Transfer Using Direct Collocation Method [Volume 1, Issue 2, 2008, Pages 35-42]

  • Naghash, Abolghasem Determining orbital element on Earth Observation Repeat-Ground-Track orbit [Volume 9, Issue 2, 2016, Pages 77-83]

  • Naghash, Abolghasem Satellite Orbit Prediction Through Observation Data and the Artificial Neural Networks [Volume 10, Issue 2, 2017, Pages 1-8]

  • Naghash, Abolghasem Flatness-based Near Optimal Guidance [Volume 10, Issue 3, 2017, Pages 15-24]

  • Naghikhani, M. Using Response Surface Method (RSM) in the Optimal Allocation of Tolerances [Volume 4, Issue 1, 2011, Pages 61-67]

  • Najafi-Asfad, M. International Humanitarian Law and Military to Take Advantage of the Space Beyond the Atmosphere [Volume 4, Issue 2, 2012, Pages 47-62]

  • Naji, H. R. FPGA Implementation of JPEG and JPEG2000-Based Dynamic Partial Reconfiguration on SOC for Remote Sensing Satellite On-Board Processing [Volume 7, Issue 1, 2014, Pages 57-66]

  • Namamian, Payman Feasibility of Implementig Criminal Jurisdiction in International Space Law [Volume 12, Issue 1, 2019, Pages 1-12]

  • Narimani, Razieh Design and Fabrication of Planar Sub-Array for Satellite Data Transmission Directive Conformal Array Antenna [Volume 17, Issue 1, 2024, Pages 73-79]

  • Naseh, H. Multi-Stage Liquid Propellant Launch Vehicle Conceptual Design, Based on Combinatorial Optimization of Major Design Parameters [Volume 1, Issue 1, 2008, Pages 21-36]

  • Naseh, H. Multi-Stage Liquid Propellant Launch Vehicle Conceptual Design (LVCD) Software, Based on Multi-Parameter Optimization Idea [Volume 1, Issue 2, 2008, Pages 17-25]

  • Naseh, H. Reliability Allocation to Launch Vehicle Subsystems by Using AHP Method in Conceptual Design Phase [Volume 5, Issue 2, 2012, Pages 49-57]

  • Naseh, H. Comprehensive Pattern in Designing Low-Thrust Space Propulsion Systems [Volume 7, Issue 3, 2014, Pages 9-21]

  • Naseh, Hasan Launch Vehicle Classical Design Software with Training Approach in Higher Education [Volume 9, Issue 3, 2016, Pages 73-79]

  • Naseh, Hasan Space Launch System Family Technology Development Model from Propulsion Aspect with Cost Approach [Volume 9, Issue 4, 2017, Pages 1-12]

  • Naseh, Hassan Optimal Mission Design for Moon Exploration Expedition [Volume 11, Issue 2, 2018, Pages 47-53]

  • Naseh, Hassan Physical Configuration Design of a 10N Monopropellant Hydrazine Thruster [Volume 12, Issue 1, 2019, Pages 13-22]

  • Naseh, Hassan Cost Estimation Model Presentation for Cryogenic/Semi-Crogenic Space Propulsion Systems [Volume 14, Issue 4, 2021, Pages 25-33]

  • Naseh, Hassan System Design and Simulation of Air-Spacecraft Aerospike Nozzle by Utilizing the Computational Fluid Dynamics (CFD) Method [Volume 16, Issue 1, 2023, Pages 23-34]

  • Naseh, Hassan Design and Configuration of Ground Sample Components of Low Propulsion Monopropellant Thruster Using Some Engineering Software [Volume 16, Issue 1, 2023, Pages 35-46]

  • Naseh, Hassan Optimized Dimension Design of Catalytic Chamber of a 10 N Thruster [Volume 16, Issue 2, 2023, Pages 55-61]

  • Naseh, Hassan Cost Estimation for Space Propulsion Systems and Human Resource Cost and The Project Implementation Time Optimization [Volume 15, Issue 3, 2022, Pages 79-92]

  • Naseh, Hassan FMECA-Based Risk Assessment in Monopropellant Hydrazine Propulsion System [Volume 16, English Special Issue, 2023, Pages 39-50]

  • Naseh, Hassan Design for reliability of a space system in the conceptual design phase [(Articles in Press)]

  • Naseh, Hassan Sensitivity Analysis Based on Progressive LHS Applied to Hydrazine Catalyst Bed Design [Volume 12, Issue 4, 2019, Pages 35-46]

  • Naseri, Siyamak Design a Model of Four Color Separation Prism in Satellite Camera [Volume 5, Issue 3, 2012, Pages 41-48]

  • Nasiri, N. Modeling and Simulating the Earth’s Magnetic Field Utilizing the 10th Generation of IGRF and Comparison the Linear and Nonlinear Transformation in order to Use in Satellite Attitude Control [Volume 3, Issue 2, 2011, Pages 45-52]

  • Nasirian, M. Simulation of Tracking Process and Communication Link with Satellite [Volume 2, Issue 3, 2009, Pages 51-56]

  • Nasirian, M. New Satellite Automatic Tracking by Doppler [Volume 8, Issue 2, 2015, Pages 57-65]

  • Nasirian, Mehrzad Satellite Passes Simulation and Calculating the Satellite Rise and Set Times for the Site [Volume 5, Issue 4, 2013, Pages 29-38]

  • Nasirian, Mehrzad Design a μ-Controller ToControl Attitude of a Flexible Microsatellite [Volume 8, Issue 1, 2015, Pages 61-71]

  • Nasrolahi, S. S. Design of Fault Detection, Isolation and Accommodation Algorithm for Attitude Determination System of a 3-Axis Satellite [Volume 5, Issue 2, 2012, Pages 1-13]

  • Navabi, M. Optimal Impulsive Maneuver Between Elliptical Coplanar-Noncoaxial Orbits [Volume 3, Issue 1, 2010, Pages 67-74]

  • Navabi, M. Modeling and Simulating the Earth’s Magnetic Field Utilizing the 10th Generation of IGRF and Comparison the Linear and Nonlinear Transformation in order to Use in Satellite Attitude Control [Volume 3, Issue 2, 2011, Pages 45-52]

  • Navabi, M. Dynamics Modeling of Spacecraft Formation Flying and Evaluating the Models Accuracy under the Effects of Relative Distance, Eccentricity and Earth Gravitational Perturbation [Volume 5, Issue 1, 2012, Pages 51-59]

  • Navabi, M. Modeling of Space Objects Propagation, Prediction of Closest Approaches among Satellites, and Assessment of Maximum Collision Probability [Volume 6, Issue 1, 2013, Pages 57-67]

  • Navabi, M. Attitude Control of Spacecraft by State Dependent Riccati Equation and Power Series Expansion of Riccati Methods [Volume 7, Issue 4, 2015, Pages 39-49]

  • Navabi, M. Nonlinear Optimal Control of Space Docking and Rendezvous Problem [Volume 8, Issue 3, 2015, Pages 27-40]

  • Navabi, M. Investigation in to The Effect of Kinematic of The Space Craft Attitude Control Using Feedback Linearization Method [Volume 11, Issue 1, 2018, Pages 59-71]

  • Navabi, M. Modeling and Control of Fuel Sloshing and its Effect on Spacecraft Attitude [Volume 11, Issue 4, 2018, Pages 11-22]

  • Navabi, M. Attitude Control of Spacecraft Using L1 Adaptive Control in the Presence of Actuator and Disturbances [Volume 13, Issue 2, 2020, Pages 79-86]

  • Navabi, M. Kinematic Modelling Without Singularity and Nonlinear Control of Satellite Attitude Using Direct Adaptive and Fuzzy PD Control Methods [Volume 14, Issue 2, 2021, Pages 77-88]

  • Navabi, M. Optimal Adaptive Control of Satellite Attitude in Presence of Uncertainty in Moment of Inertia Using Markov Parameters [Volume 13, Issue 4, 2020, Pages 25-35]

  • Navabi, M. The Turbulence Model in the Spacecraft by using A Moving Pulsed Ball Model [Volume 14, Issue 3, 2021, Pages 15-22]

  • Navabi, M. Attitude nonlinear predictive control of an under actuated spacecraft [Volume 14, Issue 4, 2021, Pages 77-83]

  • Navabi, M. Satellite Status Control Using Tabulation Gain Controller in a Variable Parameter System [Volume 15, Issue 2, 2022, Pages 15-25]

  • Navabi, M. Implementation and Comparison of Attitude Estimation Algorithms Using Low-Cost Sensors [Volume 16, Issue 2, 2023, Pages 63-77]

  • Navabi, M. الگوریتم جدید فرا ابتکاری تطبیقی در تخمین وضعیت و مدل فضاپیما [Volume 12, Issue 4, 2019, Pages 79-89]

  • Nazari, M. M. Fault Detection for an Aerospace Launch Vehicle Using Sliding Mode Observer [Volume 6, Issue 2, 2013, Pages 49-56]

  • Nazemizadeh, M. Dynamic Modeling of Flexible Manipulators Using Finite Element Method and Optimal Control of their Motion [Volume 5, Issue 2, 2012, Pages 25-34]

  • Nejat Pishkenari, Hossein Satellite 3Axis Attitude Control Using the Combination of Reaction Wheels and Thrusters [Volume 11, Issue 3, 2018, Pages 63-71]

  • Nikbakht, Vahid The Effects of Simulated Microgravity on Serum Levels of VEGF in Male Wistar Rats [Volume 9, Issue 4, 2017, Pages 63-68]

  • Nikkhah, A. A. Design and Manufacturing Steps of a Satellite Reaction Wheel [Volume 2, Issue 2, 2009, Pages 61-68]

  • Nikkhah, A. A. Optimum Transition Orbit Design for Launch Vehicles [Volume 2, Issue 3, 2009, Pages 13-17]

  • Nikkhah, A. A. Spacecraft Optimal Attitude Control by means of Reaction Wheels [Volume 2, Issue 3, 2009, Pages 35-42]

  • Nikkhah, A. A. Extracting the Non-ObservableStates in Alignment & Calibration Process for Gimballed Inertial Navigation Systems [Volume 7, Issue 3, 2014, Pages 1-8]

  • Nikkhah, A.A Attitude Stabilization and Manauvring of Agility Nanosatellite with Control Moment Gyros [Volume 7, Issue 2, 2014, Pages 1-9]

  • Nikkhah, Amie ali Simulation of Night Sky Images with an Ideal Pinhole Model for a Star Sensor [Volume 11, Issue 3, 2018, Pages 21-32]

  • Nikkhah, Amirali improve coarse alignment in inertial navigation system By the method of Identification the Kalman filter matrix [Volume 13, Issue 4, 2020, Pages 81-90]

  • Nikkhah, Amir Ali Optimal Trajectory Design of an Upper Stage for Satellite Injection into Geostationary Orbit Using Limited Thrust [Volume 9, Issue 4, 2017, Pages 13-25]

  • Nikkhah, Amir Ali Determination of the density of scattered spherical data for use in star catalog uniformity [Volume 14, Issue 2, 2021, Pages 103-110]

  • Nikkhah, Amir Ali Improved Spoofing Loosely Coupled INS /GPS with ‎Steady State Kalman Matrix Gain [Volume 16, Issue 3, 2023, Pages 37-49]

  • Niko, A.M. Design and Fabrication of Laboratory Pilot for OSL Dosimeter System for Space Applications [Volume 6, Issue 3, 2013, Pages 67-73]

  • Nikpey, Peyman GEO satellite station keeping mass design based on data mining [Volume 14, Issue 1, 2021, Pages 23-33]

  • Nikpey, Peyman Vibration Control Design of Fuel Sloshing in a Spacecraft Using Virtual Actuator [Volume 15, Issue 1, 2022, Pages 63-71]

  • Nikusokhan, M. Constrained Optimization of Launch Vehicle Trajectory Using Spline and Bezier Curves [Volume 2, Issue 2, 2009, Pages 51-60]

  • N. Meibody, Mohammad Sensitivity Analysis Based on Progressive LHS Applied to Hydrazine Catalyst Bed Design [Volume 12, Issue 4, 2019, Pages 35-46]

  • Nobahari, H. Extracting the Non-ObservableStates in Alignment & Calibration Process for Gimballed Inertial Navigation Systems [Volume 7, Issue 3, 2014, Pages 1-8]

  • Nobahari, H. Design and Real-time Implementation of the Adaptive-Neuro-Fuzzy Controller for a Temperature Control System using Model-Based Design [Volume 10, Issue 4, 2018, Pages 9-17]

  • Nobahari, Niloofar An Optimal Power Allocation in Multi-Beam Satellite Communication Systems Including Inter-Beam Interference by Particle Swarm Optimization (PSO) [Volume 10, Issue 1, 2017, Pages 55-60]

  • Nobakht Orsi, Fereydon Kinematic Standard Point Positioning (SPP) based on Kalman Filter and C/A Code Observations Under Intense Geomagnetic Storm Conditions [Volume 14, Issue 3, 2021, Pages 101-108]

  • Nobakht-Orsi, F. Spectral Analysis of Time Series of Permanent GPS Station Positions Using HHT [Volume 4, Issue 1, 2011, Pages 15-22]

  • Noorabadi, M. Governing Equations in Mechanical Analysis of Satellite Carrier Adapter [Volume 5, Issue 1, 2012, Pages 41-50]

  • Noori, S. Laminar and Turbulent Aero Heating Predictions over Blunt Body in Hypersonic Flow [Volume 7, Issue 1, 2014, Pages 33-40]

  • Noori, S. Approximate Viscous Shock-Layer Analysis of Axisymmetric Bodies in Perfect Gas Hypersonic Flow [Volume 7, Issue 1, 2014, Pages 41-48]

  • Norouz, Mohammad A Survey on Vision Navigation Methods for UAV Navigation Applications [Volume 10, Issue 2, 2017, Pages 33-52]

  • Nosrat Elahi, Mehran Integrated Design of Orbital Transfer Block in an Optimized and Multistep Converged Environment [Volume 7, Issue 4, 2015, Pages 23-37]

  • Nosrat Elahi, Mehran Solid Fuel Orbiter Designe in Optimized Space Transfer [Volume 8, Issue 1, 2015, Pages 53-60]

  • Nosratolahi, M. An Algorithm for Increasing Performance of a Space Launch Vehicle Using Solid Rocket Boosters [Volume 2, Issue 1, 2009, Pages 67-71]

  • Nosratollahi, M. Multidisciplinary Conceptual Design Optimization of Monopropellant Propulsion System of Nanosatellite [Volume 3, Issue 2, 2011, Pages 11-22]

  • Nosratollahi, M. Optimal Control Procedure for Calculating a Typical Lunch Vehicle Trajectory Based on Maximizing Payload [Volume 4, Issue 1, 2011, Pages 49-60]

  • Nosratollahi, M. Introducing of Attitude Determination System of a LEO Satellite with Orbital Maneuver Mission [Volume 4, Issue 2, 2012, Pages 1-10]

  • Nosratollahi, Mehran Performance Analysis of FMC Actuators to Microsatellite Temperature Management Based on 3-Axis and Pyramidal Configuration [Volume 13, Issue 1, 2020, Pages 49-60]

  • Nosratollahi, Mehran Design of an Upper Stage Propulsion System by Multi Objective Hybrid PSO [Volume 13, Issue 3, 2020, Pages 1-16]

  • Nosratollahi, Mehran A New Approach to Engineering Change Management for Spce Projects [Volume 14, Issue 1, 2021, Pages 43-54]

  • Nosratollahi, Mehran The presentation of the ARTA CanSat design and construction process at the CANSAT International Competition in Iran [Volume 13, Issue 2, 2020, Pages 63-77]

  • Nosratollahi, Mehran Performance evaluation of a launch vehicle with non-turbopump propulsion system based on multidisciplinary analysis (MDA) [Volume 14, Issue 4, 2021, Pages 35-49]

  • Nosratollahi, Mehran Multi-Disciplinary Optimization Conceptual Design of the Launcher Based on Non-Turbopump Propulsion Systems [Volume 15, Issue 1, 2022, Pages 121-137]

  • Nouri, S. Assessment of Solution of the Boundary Layer Equations and Approximate Relations for Aeroheating of Axisymmetric Reentry Vehicles [Volume 6, Issue 3, 2013, Pages 39-48]

  • Novinzade, A. R. Dynamic Simulation for Diffusion of Satellite Detached Particles in Various Orbits [Volume 2, Issue 1, 2009, Pages 59-65]

  • Novinzadeh, A. Design of Round Trip Trajectories to Lunar L1 [Volume 6, Issue 3, 2013, Pages 49-54]

  • Novinzadeh, A.B. Comprehensive Pattern in Designing Low-Thrust Space Propulsion Systems [Volume 7, Issue 3, 2014, Pages 9-21]

  • NOVINZADEH, ALIREZA Designing Spacecraft Attitude Control Using Model-free Optimal Control Theory [Volume 10, Issue 3, 2017, Pages 41-57]

  • N. Rahimi, H. Dynamic Modeling of Flexible Manipulators Using Finite Element Method and Optimal Control of their Motion [Volume 5, Issue 2, 2012, Pages 25-34]

O

  • Omidi, Reza Investigation and feasibility study of using components with different categories from the perspective of radiation damage in LEO and GEO orbits [Volume 14, Issue 4, 2021, Pages 11-23]

  • Omidi Gosheblagh, Reza SEU Rate and Reliability Analysis in LEO Satellites [Volume 5, Issue 3, 2012, Pages 1-9]

  • Omidi Hemmat, omid A Modification to Integral Pulse-Width Pulse-Frequency Modulator [Volume 14, Issue 1, 2021, Pages 55-64]

  • Ommi, F Microscopic Test of a Swirl Injector by High-speed Photography [Volume 10, Issue 4, 2018, Pages 1-7]

  • Ommi, F. Dual Base Swirl Injector Design for Increasing Specific Impluse in a Liquid-Fuel Rocket Engine [Volume 2, Issue 1, 2009, Pages 51-57]

  • Ommi, F. Atomyzasion Modeling the Rotating Spray Slime [Volume 4, Issue 1, 2011, Pages 39-48]

  • Ommi, F. Effective Parameters of the Aluminum Particles Cyclone Separator in the Effervescent Fuel [Volume 10, Issue 1, 2017, Pages 35-45]

  • Ommi, Fathallah Satellite Adaptive Attitude Control Based on Decentralized Minimal Control in the Presence of Reaction wheel Accurate Model [Volume 9, Issue 1, 2016, Pages 59-72]

  • Ommi, Fatholah Performance Analysis of Liquid Propellant Micro-propulsion with Liquid Oxygen as Cryogenic Oxidizer [Volume 12, Issue 1, 2019, Pages 23-40]

  • Ommi, Fatholah Numerical simulation of complicated grains with 3D burnback and Quasi-One-Dimensional flow field of solid rocket motors [Volume 12, Issue 2, 2019, Pages 23-41]

  • Ommi, Fathollah Two-dimensional numerical simulation of ablative thermal insulators in solid rocket motor combustion chamber [Volume 13, Issue 2, 2020, Pages 13-35]

  • Ommi, Fathollah Two-dimensional numerical simulation of pyrolysis and erosion in a solid rocket motor diverging-converging nozzle [Volume 14, Issue 2, 2021, Pages 1-26]

  • Ommi, Fathollah Numerical study on spray characteristic of double phases internal mix atomizer with Lagrangian approach [Volume 13, Issue 4, 2020, Pages 15-23]

  • Ommi, Fathollah Prediction of droplet size and velocity distribution based on maximum entropy formulation by nonlinear instability analysis of liquid sheet spray and turbulent of nozzle flow [Volume 13, Issue 1, 2020, Pages 1-11]

  • Ommi, Fathollah Sensitivity Analysis Based on Progressive LHS Applied to Hydrazine Catalyst Bed Design [Volume 12, Issue 4, 2019, Pages 35-46]

  • Oraee, َAshknaz Lyapunov-basedAdaptive SmoothSecond-order Sliding Mode Guidance Law with Proving Finite Time Stability [Volume 11, Issue 2, 2018, Pages 33-39]

P

  • Pahlavan, A. Studying and Calculating the Radiation Damage Caused by the Solar Radiation Spectrum in the Crystal Structure of Semiconductor Components [Volume 6, Issue 3, 2013, Pages 55-60]

  • Pakmanesh, Mohammad Reza Analysis of the Effect of Layer Perforation Pattern on the Rate of Gas Leakage from Multilayer Thermal Insulation During Satellite Launch [Volume 16, Issue 1, 2023, Pages 11-21]

  • Pariz, N. Intelligent Satellite Orbit Prediction Based on Time Series Analysis [Volume 7, Issue 3, 2014, Pages 43-49]

  • Pariz, Naser Nonlinear Dynamic Inversion Fault Tolerant Control for Spacecraft    [Volume 8, Issue 2, 2015, Pages 11-17]

  • Parsi, Behzad Verification of a Low Cost Method for Accelerometers Calibration with a Two-Axis Table [Volume 7, Issue 4, 2015, Pages 73-79]

  • ParvinJahromi, Sh. Automatic Reading of a Trade Gyrocompass Using Image Processing and Neural Networks [Volume 7, Issue 2, 2014, Pages 85-92]

  • Parviz Nowruzani, Hadi Uncertainty approach in layout design of satellite subsystems considering natural frequency constraints [Volume 14, Issue 1, 2021, Pages 65-75]

  • Payan, Meghdad Presentation of a conceptual framework for the design of Chabahar strategic launch site for the development of Iran space industry [Volume 13, Issue 1, 2020, Pages 83-98]

  • Peighani-Asl, E Electro-Optical Design of Imaging Payload for a Remote Sensing Satellite [Volume 2, Issue 3, 2009, Pages 57-70]

  • Pirzadi, Somye Improvement of Bit Error Rate (BER) in Telemetry Radio Link of Satellite LEO Using MIMO Technique [Volume 5, Issue 3, 2012, Pages 21-31]

  • Poorrajab Sufinai, Dooman Prediction of droplet size and velocity distribution based on maximum entropy formulation by nonlinear instability analysis of liquid sheet spray and turbulent of nozzle flow [Volume 13, Issue 1, 2020, Pages 1-11]

  • Pourtakdost, S. Hossein Investigation of the conduction effect on temperature-based attitude estimation [Volume 12, Issue 4, 2019, Pages 91-102]

  • Pourtakdost, S. Hossein Homotopy-based optimal trajectory design to transfer from Earth orbit to halo orbits [Volume 13, Issue 3, 2020, Pages 25-38]

  • Pourtakdost, S. Hossein Development of an Integrated Design Environment for Optimal Ascent Trajectory Planning [Volume 1, Issue 1, 2008, Pages 1-10]

  • Pourtakdoust, S. H. Optimal Coupled Spacecraft Rendezvous and Docking Using Gauss Pseudospectral Method and Step by Step Linearization [Volume 2, Issue 2, 2009, Pages 1-16]

  • Pourtakdoust, S. H. Modeling Halo Orbits and the Associated Manifolds in the Restricted Three Body Problem [Volume 3, Issue 1, 2010, Pages 75-80]

  • Pourtakdoust, S.H Optimal Multiple-Impulse Orbit Transfer Utilizing Pseudo-Newton Method [Volume 11, Issue 1, 2018, Pages 49-57]

  • Pouryavi, H. Study of Recovery System Performance of a Sounding Rocket using Launching Tests [Volume 7, Issue 2, 2014, Pages 23-33]

  • Poustini, Mohammad Javad Re-Entry Trajectory Design with Use of Aided Optimization Algorithm through Combination of Classic Guidance & Acceleration Profile Optimization [Volume 15, Issue 1, 2022, Pages 51-62]

Q

  • Qadiri Massoom, Noordin Effect of Injector Pressure Drop on The ‎Performance of A 1 N Monopropellant ‎Thruster [Volume 15, Issue 4, 2022, Pages 19-29]

  • Qadiri Massoom, Noordin Design, Fabrication, and Test of a Cryogenic Liquid Oxygen-Ethanol Engine [Volume 16, Issue 1, 2023, Pages 47-58]

R

  • Radpour, S. A Reliability Growth Model for a Launch Vehicle With its Requirements [Volume 2, Issue 1, 2009, Pages 35-42]

  • Rahbar, N. Dynamic Simulation for Diffusion of Satellite Detached Particles in Various Orbits [Volume 2, Issue 1, 2009, Pages 59-65]

  • Rahbar, Nasser Usinge The qEKF Algorithm for Satellite Attitude Estimation with Two Magnetometer & Sun Sensors [Volume 14, Issue 3, 2021, Pages 65-73]

  • Rahemi, Narjes Precise Positioning in GPS Receivers for Very High Velocities Using Combination of Recursive Least Squares and Fuzzy Logic [Volume 7, Issue 4, 2015, Pages 63-72]

  • Rahimi Ghoradel, Vahid Simulation and Parametric Analysis of Thrust Reverser System in Solid Fuel Engines [Volume 16, Issue 2, 2023, Pages 1-17]

  • Rahmanian, Narjes Effect of Simulated Microgravity Condition on Cells Proliferation and Myostatin Gene Expression in Differentiated Skeletal Muscle Cells (C2C12) [Volume 15, Issue 2, 2022, Pages 81-92]

  • Raisali, Gholamreza Determination of the Sensitive Volume and Critical Charge for Induction of SEU in Nanometer SRAMs [Volume 16, Issue 2, 2023, Pages 43-54]

  • Raisi, K. Designing and Constructing of Inverted F Antennas on a Space Bound Vehicle for Telemetry Transmission [Volume 1, Issue 2, 2008, Pages 57-60]

  • Raissi, K. Considerations of Utilizing Telemetry and GPS System in Sounding Rockets [Volume 1, Issue 1, 2008, Pages 81-86]

  • Rajabi, Alireza Investigation on Performance Characteristics of Hydrazine Monopropellant Thruster according to Reaction Chamber Adiabatic Temperature [Volume 15, Issue 3, 2022, Pages 33-47]

  • Rajabi, Alireza Effect of Injector Pressure Drop on The ‎Performance of A 1 N Monopropellant ‎Thruster [Volume 15, Issue 4, 2022, Pages 19-29]

  • Ramesh, D. Study of Hot Gas Pressurizing System Tank and Liquid Rocket Engine Interaction by Dynamic Simulation [Volume 6, Issue 1, 2013, Pages 11-19]

  • Ramesh, D. Dynamics Simulation of Pressurizing in Propulsion System Configuration [Volume 6, Issue 3, 2013, Pages 1-13]

  • Ramesh, D. Neural Network Based Diagnostic Indication of a Liquid Propellant Engine with Faulty Data Collection System [Volume 7, Issue 2, 2014, Pages 75-83]

  • Ramesh, Davood Optimization of Schematic and Parameters of Staged Combustion Launch Vehicle Liquid Engines [Volume 9, Issue 1, 2016, Pages 1-11]

  • Ramesh, Davood Dynamic & Non-linear Modelling of an Expansion Cycle Rocket Engine [Volume 13, Issue 1, 2020, Pages 39-48]

  • Ramezani, Alireza Investigation of a Bi-propellant Thruster by a Developed Space Engine’s Thrust Chamber Analysis Code [Volume 14, Issue 2, 2021, Pages 47-37]

  • Ramezani, Morteza Modeling the Solar Array Design of Remote Sensing Satellites Based on Adaptive Neuro-Fuzzy Inference System [Volume 11, Issue 3, 2018, Pages 1-8]

  • Ramezani Najafi, Hamed Analysis of the Effect of Layer Perforation Pattern on the Rate of Gas Leakage from Multilayer Thermal Insulation During Satellite Launch [Volume 16, Issue 1, 2023, Pages 11-21]

  • Ramezani-Najafi, Hamed Design and Manufacture of Thermal Model of AUTSAT Satellite and Its Thermal Balance Test [Volume 9, Issue 2, 2016, Pages 61-76]

  • Ranjbar, Javad Extensive Regional Telecommunications Coverage in Emergency Condition Using Tethered-Balloon Equipped with Antenna Pointing Mechanism – Part 1: Kinematic and Dynamic Modeling [Volume 15, Issue 2, 2022, Pages 27-41]

  • Ranjbar, Javad Extensive Regional Telecommunications Coverage in Emergency Condition Using Satellite and Tethered-Balloon Equipped with Antenna Pointing Mechanism – Part 2: Operation Modes and Controller Design [Volume 15, Issue 4, 2022, Pages 71-88]

  • RashedMohasal, Jalil Space Application of a Linear Array of Plasma Antenna [Volume 5, Issue 3, 2012, Pages 59-66]

  • Rashidi, Ali Jabbar Design of a Multiband and Wide Angle Reflector [Volume 12, Issue 4, 2019, Pages 47-56]

  • RasiMarzabadi, F. Study of Recovery System Performance of a Sounding Rocket using Launching Tests [Volume 7, Issue 2, 2014, Pages 23-33]

  • Razipour, Fariba International Humanitarian Law and Military to Take Advantage of the Space Beyond the Atmosphere [Volume 4, Issue 2, 2012, Pages 47-62]

  • Razmjooei, Mohammad Two-dimensional numerical simulation of pyrolysis and erosion in a solid rocket motor diverging-converging nozzle [Volume 14, Issue 2, 2021, Pages 1-26]

  • Refan, Mohammad Hossein Improving DGPS Accuracy Using Predictions of Reference Position Components Error Factors [Volume 8, Issue 2, 2015, Pages 41-56]

  • Reyvandi, A. SAR Imaging Systems Performance Modeling [Volume 6, Issue 1, 2013, Pages 47-56]

  • Rezaee, Alireza An Optimal Power Allocation in Multi-Beam Satellite Communication Systems Including Inter-Beam Interference by Particle Swarm Optimization (PSO) [Volume 10, Issue 1, 2017, Pages 55-60]

  • Rezaei, Mahmoud Reza Star Sensor Relative Accuracy Measurement in Night Sky [Volume 13, Issue 3, 2020, Pages 79-89]

  • Rezaei, Mohammad Study of The Most Important Applications of Local Positioning System (LPS) In Iran [Volume 11, Issue 3, 2018, Pages 33-45]

  • Rezaeian Parsa, E. Effects of Erosive Burning on Solid Rocket Motor Internal Ballistics [Volume 5, Issue 2, 2012, Pages 69-74]

  • Rezaiha, A. Design and Manufacturing a Laboratory Example of Pulsed Plasma Thruster [Volume 3, Issue 2, 2011, Pages 23-30]

  • Rivandi, Mahdi Design and Implementation of a Balance System for the CubeSat Attitude Determination and Control Tabletop Simulator [Volume 16, Issue 1, 2023, Pages 75-88]

  • R. Najafi, Hamed Evaluation of Effective Emissivity of a Multilayer Insulation Blanket Using Test [Volume 8, Issue 1, 2015, Pages 19-25]

  • Roghangir, seyed Amirreza Orbit Determination via a Deeply- Coupled UKF/GNSS Filter [Volume 9, Issue 3, 2016, Pages 13-26]

  • Rohami, Rohollah The current framework of Space Law approach to commercial space activities: prescriptive or restrictive [Volume 13, Issue 1, 2020, Pages 25-38]

  • Roshanian, J. Multidisciplinary Design Optimization of a Small Launch Vehicle; a System Sensitivity Analysis Approach [Volume 1, Issue 1, 2008, Pages 47-56]

  • Roshanian, J. Flexible Spacecraft Attitude Control using Hybrid Control Scheme of H∞ and Sliding Mode Control [Volume 1, Issue 2, 2008, Pages 51-56]

  • Roshanian, J. Flexible Spacecraft Three Axis Attitude Maneuver by Active Vibration Control [Volume 2, Issue 1, 2009, Pages 43-50]

  • Roshanian, J. Constrained Optimization of Launch Vehicle Trajectory Using Spline and Bezier Curves [Volume 2, Issue 2, 2009, Pages 51-60]

  • Roshanian, J. کاربرد مدل پاندول ساده به منظور اعمال دینامیک تلاطم سیال در شبیه‌سازی شش درجه آزادی پرواز ماهواره‌بر [Volume 3, Issue 2, 2011, Pages 59-67]

  • Roshanian, J. Required Velocity Calculation in the Presence Of Atmosphere Effect in C* Matrix [Volume 4, Issue 1, 2011, Pages 69-78]

  • Roshanian, J. Survey on Nondeterministic Optimal Design and Its Applications in the Aerospace Industry [Volume 4, Issue 2, 2012, Pages 23-34]

  • Roshanian, J. Developing Attitude Control for Suborbital Module Based on Cold Gas Thrusters and Using Quaternion Feedback [Volume 6, Issue 1, 2013, Pages 1-10]

  • Roshanian, J. Fault Detection for an Aerospace Launch Vehicle Using Sliding Mode Observer [Volume 6, Issue 2, 2013, Pages 49-56]

  • Roshanian, J. Space Inertial Navigation System Accuracy Increasing Using Orbit Point Mass Dynamic [Volume 6, Issue 2, 2013, Pages 57-66]

  • Roshanian, J. Developing a New Explicit Guidance Method for the Trajectory Correction of Sub-Orbital Modules [Volume 6, Issue 3, 2013, Pages 15-26]

  • Roshanian, J. Developing a Multi-Objective Guidance Scenario for the Entry to the Earth’s Atmosphere [Volume 6, Issue 4, 2014, Pages 53-62]

  • Roshanian, J. Attitude Stabilization and Manauvring of Agility Nanosatellite with Control Moment Gyros [Volume 7, Issue 2, 2014, Pages 1-9]

  • Roshanian, Jafar Consideration on Actualizing the Non-Dimensional Star Pattern Recognition Algorithm for a Typical Laboratory Star Tracker [Volume 5, Issue 2, 2012, Pages 15-23]

  • Roshanian, Jafar Star Catalog Criteria Selection and Mission Catalog Update for a Typical Star Tracker [Volume 5, Issue 4, 2013, Pages 1-8]

  • Roshanian, Jafar Combining Gradient and Evolutionary Algorithms for Improving Collaborative Optimization Performance [Volume 8, Issue 2, 2015, Pages 27-39]

  • Roshanian, Jafar Online Optimal Integrated Guidance and Control Algorithm Design for Launch Vehicle [Volume 8, Issue 2, 2015, Pages 67-78]

  • Roshanian, Jafar Optimal Trajectory Design of an Upper Stage for Satellite Injection into Geostationary Orbit Using Limited Thrust [Volume 9, Issue 4, 2017, Pages 13-25]

  • Roshanian, Jafar Simulation of Night Sky Images with an Ideal Pinhole Model for a Star Sensor [Volume 11, Issue 3, 2018, Pages 21-32]

  • Roshanian, Jafar Analytical Solution to relative dynamic of gravity tractors in Formation Flying in Asteroid Deflection Mission [Volume 11, Issue 4, 2018, Pages 31-42]

  • Roshanian, Jafar Determination of the density of scattered spherical data for use in star catalog uniformity [Volume 14, Issue 2, 2021, Pages 103-110]

  • Roshanian, Jafar Hybrid PID-FUZZY Control of Formation Flying of Spacecrafts in order to asteroid Deflection Mission [Volume 12, Issue 4, 2019, Pages 19-33]

  • Roshanyan, Jafar Integrated Inertial Navigation with Positioning System for Increasing Orbital Module Navigation Accuracy [Volume 5, Issue 3, 2012, Pages 11-19]

  • Roshnian, J. Comparison Between Traditional Method (Statistical Method) and Multidisciplinary Optimization Method (AAO) in Designing of a Lightweight Liquid Propellant LV [Volume 5, Issue 1, 2012, Pages 61-72]

  • Rostami, Mohsen Numerical Study on the Effects of Nozzle Geometry and Creating Swirly Flow Inside the Injector Nozzle on the Performance of an Engine [Volume 15, Issue 4, 2022, Pages 107-121]

  • Rouholamini, Seyyed Rashad Investigation on Performance Characteristics of Hydrazine Monopropellant Thruster according to Reaction Chamber Adiabatic Temperature [Volume 15, Issue 3, 2022, Pages 33-47]

  • Rouholamini, Seyyed Rashad Effect of Injector Pressure Drop on The ‎Performance of A 1 N Monopropellant ‎Thruster [Volume 15, Issue 4, 2022, Pages 19-29]

  • Rouholamini, S. Rashad Design, Fabrication, and Test of a Cryogenic Liquid Oxygen-Ethanol Engine [Volume 16, Issue 1, 2023, Pages 47-58]

S

  • Saadat dar, Ali The presentation of the ARTA CanSat design and construction process at the CANSAT International Competition in Iran [Volume 13, Issue 2, 2020, Pages 63-77]

  • Saadat dar, Ali Introducing the conceptual design process of the Armita lunar rover Based on ECSS [(Articles in Press)]

  • Sabahi, Mohammad Farzan Using the Joint Probabilistic Data Association Filter for Improving Star Trackers Performance to Accurate Attitude Determination of Spacecrafts [Volume 9, Issue 1, 2016, Pages 37-46]

  • Sabatifar, M. Optimal Impulsive Maneuver Between Elliptical Coplanar-Noncoaxial Orbits [Volume 3, Issue 1, 2010, Pages 67-74]

  • Saberali, Sayed Mohamad Using the Joint Probabilistic Data Association Filter for Improving Star Trackers Performance to Accurate Attitude Determination of Spacecrafts [Volume 9, Issue 1, 2016, Pages 37-46]

  • Saberi-Tavakoli, Mohammad Collision-Free Control for Multiple Satellites via Formation Feedback of Virtual Structure [Volume 5, Issue 4, 2013, Pages 47-60]

  • Sabeti, MohammadReza A New Approach to Engineering Change Management for Spce Projects [Volume 14, Issue 1, 2021, Pages 43-54]

  • Saboohi, Zoheir Performance Analysis of Liquid Propellant Micro-propulsion with Liquid Oxygen as Cryogenic Oxidizer [Volume 12, Issue 1, 2019, Pages 23-40]

  • Saboohi, Zoheir Design of a Diffuser for a Subsonic Wind Tunnel Using CFD [Volume 12, Issue 3, 2019, Pages 1-13]

  • Sadati, Seyed Hossein Re-Entry Trajectory Design with Use of Aided Optimization Algorithm through Combination of Classic Guidance & Acceleration Profile Optimization [Volume 15, Issue 1, 2022, Pages 51-62]

  • Sadeghi, Ahmad Reza Using the Joint Probabilistic Data Association Filter for Improving Star Trackers Performance to Accurate Attitude Determination of Spacecrafts [Volume 9, Issue 1, 2016, Pages 37-46]

  • Sadeghi, H. Design and Fabrication of Laboratory Pilot for OSL Dosimeter System for Space Applications [Volume 6, Issue 3, 2013, Pages 67-73]

  • Sadeghi, Milad The Intellectual Property Rights and Transfer of Technology in Space Industry [Volume 15, Issue 1, 2022, Pages 107-119]

  • Sadeghi Givi, Z. Considerations of Utilizing Telemetry and GPS System in Sounding Rockets [Volume 1, Issue 1, 2008, Pages 81-86]

  • Sadeghi-kia, fatemeh Plasma Antenna Technology in Space Missions [Volume 10, Issue 1, 2017, Pages 27-34]

  • Sadeghikia, F. Designing and Constructing of Inverted F Antennas on a Space Bound Vehicle for Telemetry Transmission [Volume 1, Issue 2, 2008, Pages 57-60]

  • Sadeghikia, Fateme Space Application of a Linear Array of Plasma Antenna [Volume 5, Issue 3, 2012, Pages 59-66]

  • Sadeghikia, Fatemeh Low-Profile Helical Antenna for Space Application [Volume 11, Issue 2, 2018, Pages 55-59]

  • Sadeghikia, Fatemeh Thermal Effects of the Space Environment on the Radiation Characteristics of a Reflector Antenna in LEO Satellite [Volume 15, Issue 2, 2022, Pages 103-113]

  • Sadeghikia, Fatemeh A Reconfigurable and Steerable Horn Antenna Using Plasma Dielectric Slabs for Controllable Gain and Beam Steering [(Articles in Press)]

  • Sadeghzade, Ali Conformal Anti Jamming GPS Antenna with Directive Elements [Volume 13, Issue 3, 2020, Pages 63-68]

  • Sadidi, Javad Data Augmentation Investigating in Improving the performance of Deep Learning Model for Building Segmentation using Aerial Images [Volume 15, Issue 3, 2022, Pages 23-32]

  • Sadr, Ali Analysis, Design and Optimization of the Multi Layer Radiation Shielding of Satellite Electronic Components [Volume 14, Issue 2, 2021, Pages 71-76]

  • Saeed Farzaneh, Saeed An Adaptive Method for Star Extraction from Digital Astronomical Images [Volume 2, Issue 2, 2009, Pages 27-38]

  • Saeidi, Abbas Usinge The qEKF Algorithm for Satellite Attitude Estimation with Two Magnetometer & Sun Sensors [Volume 14, Issue 3, 2021, Pages 65-73]

  • Safaei, Nazanin Optimal Adaptive Control of Satellite Attitude in Presence of Uncertainty in Moment of Inertia Using Markov Parameters [Volume 13, Issue 4, 2020, Pages 25-35]

  • Safaei Hashekvaei, Nazanin Kinematic Modelling Without Singularity and Nonlinear Control of Satellite Attitude Using Direct Adaptive and Fuzzy PD Control Methods [Volume 14, Issue 2, 2021, Pages 77-88]

  • Safari, Abdolreza Kinematic Standard Point Positioning (SPP) based on Kalman Filter and C/A Code Observations Under Intense Geomagnetic Storm Conditions [Volume 14, Issue 3, 2021, Pages 101-108]

  • Safari, A. R. Spectral Analysis of Time Series of Permanent GPS Station Positions Using HHT [Volume 4, Issue 1, 2011, Pages 15-22]

  • Safarinejad, Behrooz Presentation of the structure of an Inertial Measurement Unit to evaluate the rotation without using gyros [Volume 13, Issue 3, 2020, Pages 69-77]

  • Safavi Homami, M. Total Ionizing Dose Test on AT90CAN128 MicroController [Volume 6, Issue 4, 2014, Pages 63-67]

  • Safdarinezhad, Alireza A method for determining the optimum parameter of the soft filters to image fusion in the frequency domain [Volume 14, Issue 3, 2021, Pages 23-37]

  • Saghafi, Fariborz Collision-Free Control for Multiple Satellites via Formation Feedback of Virtual Structure [Volume 5, Issue 4, 2013, Pages 47-60]

  • Saghari, A. Comprehensive Code of Remote Sensing Satellite Conceptual Design [Volume 7, Issue 2, 2014, Pages 35-47]

  • Saghari, Asad Complementary Method the Conceptual Design of Space Craft Electrical Power  Subsystem [Volume 8, Issue 3, 2015, Pages 55-63]

  • Saghari, Asad Determine the Optimal Orbit for an Earth Observation Satellite Considering the Power [Volume 9, Issue 3, 2016, Pages 27-36]

  • Saghari, Asad Design and sensitivity analysis of an Earth observation mission's operating orbit in the absence of injection into the Sun-synchronous orbit [Volume 14, Issue 4, 2021, Pages 1-9]

  • Sajjad, Niki Development of MIL and PIL testbed for Student Microsatellite Attitude Control Subsystem [Volume 13, Issue 3, 2020, Pages 51-62]

  • Salari, Mohammad Design and manufacturing of the antenna motion mechanisms of a communication satellite [Volume 12, Issue 2, 2019, Pages 43-53]

  • Salarieh, Hassan Attitude Control of Nanosatellite Using Optimal Quadratic Linear and Nonlinear Methods [Volume 16, English Special Issue, 2023, Pages 51-64]

  • Salavatifar, Maryam CD44 expression changes in MDA-MB-231 cell line of breast cancer after exposure to 2-D clinorotation [Volume 14, Issue 4, 2021, Pages 61-66]

  • Salavatifar, Maryam Heterologous Expression of Shiga-Like Toxin Type 2 in Microgravity Condition [Volume 15, Issue 4, 2022, Pages 97-106]

  • Saleh, R. Simulation of Tracking Process and Communication Link with Satellite [Volume 2, Issue 3, 2009, Pages 51-56]

  • Salehghaffari, H. Hybrid Estimation of Gyro Model Parameters and GEO Satellite Moment of Inertia with Extended Kalman Filter [Volume 6, Issue 2, 2013, Pages 67-74]

  • Salehi, M. Implementation and Comparison of Attitude Estimation Algorithms Using Low-Cost Sensors [Volume 16, Issue 2, 2023, Pages 63-77]

  • SalehiAmiri, S. M. Extracting the Non-ObservableStates in Alignment & Calibration Process for Gimballed Inertial Navigation Systems [Volume 7, Issue 3, 2014, Pages 1-8]

  • Salehy, Saeid Multi objective design optimization of heat pipes configuration attached to the solar panels of a sun pointing satellite [Volume 12, Issue 1, 2019, Pages 55-68]

  • Salem, Javad Reduce Position and Velocity RMS Error of Non-linear Filters in LEO Satellite Radar Tracking [Volume 9, Issue 4, 2017, Pages 51-63]

  • Salimi, A Satellite Attitude Control by Magnetic Torquers with Variable Magnetic Intensity for Optimization of Power Consumption [Volume 1, Issue 1, 2008, Pages 37-45]

  • Salimi, Mohammad Reza Equilibrium Effects on the Hypersonic Laminar Boundary Layer Flow over Axisymmetric Bodies [Volume 8, Issue 4, 2016, Pages 19-27]

  • Salimi, Mohammad Reza Physical Configuration Design of a 10N Monopropellant Hydrazine Thruster [Volume 12, Issue 1, 2019, Pages 13-22]

  • Salimi, Mohammad Reza Effects of Geometrical Parameters of a Two-Sided Catalyst Bed on Flow and Thermal Fields of a Monopropellant Hydrazine Thruster [Volume 15, Issue 1, 2022, Pages 89-105]

  • Salimi, Mohammad Reza Design, Construction and Performance Evaluation of a Cold Gas Thruster Test Stand [Volume 15, English Special Issue, 2022, Pages 55-64]

  • Salimi, Mohammad Reza Numerical Study on the Effects of Nozzle Geometry and Creating Swirly Flow Inside the Injector Nozzle on the Performance of an Engine [Volume 15, Issue 4, 2022, Pages 107-121]

  • Salimi, Mohammad Reza Design and Configuration of Ground Sample Components of Low Propulsion Monopropellant Thruster Using Some Engineering Software [Volume 16, Issue 1, 2023, Pages 35-46]

  • Salimi, Mohammad Reza Optimized Dimension Design of Catalytic Chamber of a 10 N Thruster [Volume 16, Issue 2, 2023, Pages 55-61]

  • Salimi, M. R. Assessment of Solution of the Boundary Layer Equations and Approximate Relations for Aeroheating of Axisymmetric Reentry Vehicles [Volume 6, Issue 3, 2013, Pages 39-48]

  • Salmanian, Ali Hatef Heterologous Expression of Shiga-Like Toxin Type 2 in Microgravity Condition [Volume 15, Issue 4, 2022, Pages 97-106]

  • Samadi Khoshkho, Zahra Satellite Adaptive Attitude Control Based on Decentralized Minimal Control in the Presence of Reaction wheel Accurate Model [Volume 9, Issue 1, 2016, Pages 47-56]

  • Samadzadegan, F. An Adaptive Method for Star Extraction from Digital Astronomical Images [Volume 2, Issue 2, 2009, Pages 27-38]

  • Samadzadegan, F. Automatic Navigation of Aerial Vehicles on a Vision-Aided Navigation System [Volume 5, Issue 1, 2012, Pages 1-14]

  • Samipour, Sadjad A Method for Determining Design Parameters of Space Umbrella Antenna [Volume 15, Issue 4, 2022, Pages 31-43]

  • Sangary, Arash Integrated Inertial Navigation with Positioning System for Increasing Orbital Module Navigation Accuracy [Volume 5, Issue 3, 2012, Pages 11-19]

  • SarAbadani, Atiyeh Investigation of a Bi-propellant Thruster by a Developed Space Engine’s Thrust Chamber Analysis Code [Volume 14, Issue 2, 2021, Pages 47-37]

  • Sargolzaie, Mohsen Experimental Study of Dynamic Stability for a Entry Capsule in Supersonic Flow [Volume 15, Issue 2, 2022, Pages 71-80]

  • Sayahnia, R. Remote Sensing Role in Land Use StudiesCase Study: Tehran Metropolitan and its Boundary [Volume 7, Issue 3, 2014, Pages 69-73]

  • Sayanjali, M. Flexible Spacecraft Attitude Control using Hybrid Control Scheme of H∞ and Sliding Mode Control [Volume 1, Issue 2, 2008, Pages 51-56]

  • Sayanjali, M. Flexible Spacecraft Three Axis Attitude Maneuver by Active Vibration Control [Volume 2, Issue 1, 2009, Pages 43-50]

  • Sayanjali, Mohammad Optimal Multiple-Impulse Orbit Transfer Utilizing Pseudo-Newton Method [Volume 11, Issue 1, 2018, Pages 49-57]

  • Sayanjali, Mohammad Homotopy-based optimal trajectory design to transfer from Earth orbit to halo orbits [Volume 13, Issue 3, 2020, Pages 25-38]

  • Sedaghat, H. Automatic Star Identification Using Triangle Base and Increase Search Speed [Volume 4, Issue 2, 2012, Pages 83-92]

  • Seddighi renani, Neda sadat Developing a Universal Software for the Conceptual Design of Cryogenic Rocket Propulsion System [Volume 15, Issue 1, 2022, Pages 73-87]

  • Sedghi, V. Total Ionizing Dose Test on AT90CAN128 MicroController [Volume 6, Issue 4, 2014, Pages 63-67]

  • Sedighi, S. Hasan Conformal Anti Jamming GPS Antenna with Directive Elements [Volume 13, Issue 3, 2020, Pages 63-68]

  • Sedighi, S. Hassan Design and Fabrication of a dual-polar reflector array antenna for satellite applications [Volume 13, Issue 2, 2020, Pages 99-104]

  • Sedighi, S. Hassan Design and Optimization of Satellite Telecommunication Relay Using Pseudo-Noise Ranging [Volume 15, Issue 4, 2022, Pages 45-56]

  • Sedigh Koochaki, Mehrdad FMECA-Based Risk Assessment in Monopropellant Hydrazine Propulsion System [Volume 16, English Special Issue, 2023, Pages 39-50]

  • Sedighy, Seyed Hassan Design and Fabrication of Planar Sub-Array for Satellite Data Transmission Directive Conformal Array Antenna [Volume 17, Issue 1, 2024, Pages 73-79]

  • Sedighy, S. Hasan Analysis, Design and Optimization of the Multi Layer Radiation Shielding of Satellite Electronic Components [Volume 14, Issue 2, 2021, Pages 71-76]

  • Sefidan Benisi, Arash A Nonlinear Attitude Controller for a Launch Abort System of a Manned Spacecraft [Volume 10, Issue 1, 2017, Pages 1-13]

  • Seyedzamani, Soheil HIL Experimental Analyses of Satellite Electrical Power Subsystem (EPS) in De-tumbling Mode [Volume 10, Issue 4, 2018, Pages 19-28]

  • Seyedzamani, Soheil Damping mode of satellite angular velocity using magnetic actuators in hardware/software in the loop [Volume 12, Issue 4, 2019, Pages 57-67]

  • Seyedzamani, Soheil Design and implementation of hardware-in-the-loop (HIL) test-bed for spacecraft attitude control [Volume 12, Issue 2, 2019, Pages 55-70]

  • Shaabani, Keyvan Design, Manufacture and Experimental Study of a Hydrogen Peroxide-HTPB Hybrid Rocket Motor [Volume 5, Issue 4, 2013, Pages 19-28]

  • Shafieenejad, Iman Spacecraft Trajectory Design Regarding Van Allen Belts by Honey Bee Optimisation Algorithm [(Articles in Press)]

  • Shafiee-Nejhad, E. Dynamic Simulation for Diffusion of Satellite Detached Particles in Various Orbits [Volume 2, Issue 1, 2009, Pages 59-65]

  • Shafiei, Mohammad Hosein Velocity and Body Rate Control of a Spacecraft Using Robust Passivity-Based Control [Volume 11, Issue 2, 2018, Pages 41-46]

  • Shafiei, Mohammad Hosein Presentation of the structure of an Inertial Measurement Unit to evaluate the rotation without using gyros [Volume 13, Issue 3, 2020, Pages 69-77]

  • Shafiei, Mohammad Hosein Robust Three-Dimensional Guidance Law Design against Maneuvering Targets with Approach of Discrete-time Partial Stabilization [Volume 12, Issue 3, 2019, Pages 55-61]

  • Shafiei, Mohammad Hossein New Approach in Guidance Law Design Based on Finite-Time Partial Stability Theorem [Volume 8, Issue 1, 2015, Pages 1-7]

  • Shafiey Dehaj, M. Modeling of Shutdown Process in Liquid Propellant Rocket Engines [Volume 6, Issue 4, 2014, Pages 1-11]

  • Shahanaghi, K. Designing an Estimation Pattern for Reliability of Launch Vehicle Structure with Bayesian Networks [Volume 5, Issue 1, 2012, Pages 73-80]

  • Shahbahrami, Valiollah Attitude and Vibration Control of a Flexible Spacecraft Using Hybrid Adaptive Super-Twisting Non-Singular Terminal Sliding Mode Control [Volume 16, Issue 4, 2023, Pages 1-13]

  • Shahbazi, Mohammad Two-dimensional numerical simulation of pyrolysis and erosion in a solid rocket motor diverging-converging nozzle [Volume 14, Issue 2, 2021, Pages 1-26]

  • Shahgoli, B. Automatic Reading of a Trade Gyrocompass Using Image Processing and Neural Networks [Volume 7, Issue 2, 2014, Pages 85-92]

  • Shahidzadeh, Saber Determining Allowed Positions of Aeronautical-Earth Station in Motion (A-ESIM) Prevent its Frequency Interference in the Fixed Ground Station [Volume 16, Issue 3, 2023, Pages 1-14]

  • Shahmirzai Jashoghani, S. Optimal Control Procedure for Calculating a Typical Lunch Vehicle Trajectory Based on Maximizing Payload [Volume 4, Issue 1, 2011, Pages 49-60]

  • Shahravi, Majid Identification of Space Deployable Mechanisms [Volume 9, Issue 3, 2016, Pages 53-71]

  • Shahravi, Morteza Designing and Evaluation of an Experimental Attitude Determination System Using Sun Sensor and Magnetometer [Volume 5, Issue 4, 2013, Pages 69-78]

  • Shahri Razlighi, Alireza The magnetic cleanliness of a satellite Based on optimum placement of equipment using PSO [Volume 14, Issue 2, 2021, Pages 61-69]

  • Shahriyari, M. Determination of Deployment Angle for the Optimum Operation of Solar Panels Used in a LEO Satellite [Volume 1, Issue 2, 2008, Pages 1-8]

  • Shahryari ‎, Mehran Thermal Modeling of Lidar Payload in a Remote Sensing Satellite under System Level Considerations with a Review on its Challenges [Volume 16, Issue 2, 2023, Pages 79-91]

  • Shakouri, Amir Optimal Multiple-Impulse Orbit Transfer Utilizing Pseudo-Newton Method [Volume 11, Issue 1, 2018, Pages 49-57]

  • Shamadi, Yosef Guidance and Control for Space Capsule in the Presence of Uncertain Dynamic Parameters during the Atmospheric Entry Phase [Volume 8, Issue 3, 2015, Pages 1-13]

  • Shamim, Farhad Design and Manufacturing of a Variable Speed Control Moment Gyro for an Agile Micro-Satellite Attitude Control Simulator [Volume 8, Issue 1, 2015, Pages 73-77]

  • Shamirzaei, Mohsen Inertial navigation position error estimation, using vision system [Volume 14, Issue 3, 2021, Pages 75-90]

  • Shams, Javad Analytical Solution to relative dynamic of gravity tractors in Formation Flying in Asteroid Deflection Mission [Volume 11, Issue 4, 2018, Pages 31-42]

  • Shams, Javad Hybrid PID-FUZZY Control of Formation Flying of Spacecrafts in order to asteroid Deflection Mission [Volume 12, Issue 4, 2019, Pages 19-33]

  • Sharifi, Alireza Design and Real-time Implementation of the Adaptive-Neuro-Fuzzy Controller for a Temperature Control System using Model-Based Design [Volume 10, Issue 4, 2018, Pages 9-17]

  • Sharifi, Alireza Rapid Performance Sizing of Reaction Wheels in a Very High Resolution Remote Sensing Satellite Using Matching Diagram Technique [Volume 15, Issue 1, 2022, Pages 21-39]

  • Sharifi, Ali Reza Comparison of Direct and Indirect Georeferencing Methods Using Satellite Linear Array Iimages [Volume 8, Issue 2, 2015, Pages 1-10]

  • Sharifi, M. A. An Adaptive Method for Star Extraction from Digital Astronomical Images [Volume 2, Issue 2, 2009, Pages 27-38]

  • Sharifi, M. A. Spectral Analysis of Time Series of Permanent GPS Station Positions Using HHT [Volume 4, Issue 1, 2011, Pages 15-22]

  • Sharifi, Mohammad Ali The Retrieval of Wet Refractivity Index by Tomography Using Spherical Cap Harmonics [Volume 15, English Special Issue, 2022, Pages 15-24]

  • Sharifi, S. M. M. Designing an Estimation Pattern for Reliability of Launch Vehicle Structure with Bayesian Networks [Volume 5, Issue 1, 2012, Pages 73-80]

  • Sharifi Hafshejani, Reza High Precision Remote Sensing Payload Alignment Procedure Using Theodolite and Alignment Cube [Volume 16, Issue 1, 2023, Pages 1-9]

  • Sharifzadeh, Reza Microscopic Test of a Swirl Injector by High-speed Photography [Volume 10, Issue 4, 2018, Pages 1-7]

  • Shefaee Roshan, Maziar Control Allocation for Redundant Thruster of a Spacecraft via Direction-Preserving Approach in Simplex Algorithm [Volume 13, Issue 1, 2020, Pages 71-82]

  • Sheida, M. Assessment of Solution of the Boundary Layer Equations and Approximate Relations for Aeroheating of Axisymmetric Reentry Vehicles [Volume 6, Issue 3, 2013, Pages 39-48]

  • Sheikhbahaei, Reza Optimal Proportional Navigation in Three-Dimensional Space Using Model Predictive Control Approach [Volume 14, Issue 4, 2021, Pages 51-59]

  • Sheikhi, Abbas Design of a Multiband and Wide Angle Reflector [Volume 12, Issue 4, 2019, Pages 47-56]

  • Shekoofa, O. Evaluation of the Impacts of Orbit Parameters Change on Specifications and Performance of Power Sources of LEO Satellites [Volume 2, Issue 2, 2009, Pages 39-49]

  • Shekoofa, Omid System-level Evaluation of the Operation of Different Solar Array Structures for Various CubeSat Configurations [Volume 15, Issue 3, 2022, Pages 93-108]

  • Shojaee, R. Simulation of Tracking Process and Communication Link with Satellite [Volume 2, Issue 3, 2009, Pages 51-56]

  • Shojaee, T. Attitude Control System Design Based on Fluidic Momentum Controllers under Adaptive Sliding Mode [Volume 7, Issue 2, 2014, Pages 63-74]

  • Shokrieh, M. M. Design and Aanalysis of Sandwich Panels as a Support Structure of Solar Cells for a GEO Communications Satellite [Volume 6, Issue 4, 2014, Pages 13-22]

  • Shokrolahi, Pourya Applying multi-objective optimization approaches to design an optimal controller for orbital docking by consideration of actuators dynamics and comparing results [Volume 13, Issue 2, 2020, Pages 87-96]

  • Shoorian, Sara Calculation and measurement of leakage current variations due to displacement damage for a silicon diode exposed to space protons [Volume 13, Issue 4, 2020, Pages 71-79]

  • Shoorian, Sara Using Space Radiation Shielding Made of Polyethylene Instead of Aluminum in GEO Orbit to Reduce Weight [Volume 16, Issue 4, 2023, Pages 15-27]

  • Shoorian, Sarah Studying the Effects of Multi-Layer Shielding in Reducing Space Radiations Exposure of Human and Electrical Components in Space Missions [Volume 16, Issue 2, 2023, Pages 19-26]

  • Siami, Ehsan Evaluation of Changes in the Expression Level of some Genes Involved in Decompression Sickness in the Pressure Changes [Volume 15, Issue 1, 2022, Pages 41-49]

  • Smailzadeh, S. M. Satellite Thermal Modeling and Analysis with the Electrical Network Method [Volume 5, Issue 1, 2012, Pages 81-90]

  • Sohrab, M. Ascending Phase Fuzzy Logic Guidance of Satellite Launch Vehicles for Reducing the Adverse Wind Effects [Volume 7, Issue 3, 2014, Pages 75-82]

  • Sojoodi, Parvin Investigating the Test and Evaluation of GaN Transistors Radiation Resistance in SSPA Amplifier Board in LEO Satellite Payload [Volume 16, Issue 1, 2023, Pages 59-74]

  • Sojoodi, Parvin Gap Analysis in Satellite Communication Services [Volume 16, Issue 4, 2023, Pages 29-40]

  • Soleimani, Ahmad Performance Analysis of FMC Actuators to Microsatellite Temperature Management Based on 3-Axis and Pyramidal Configuration [Volume 13, Issue 1, 2020, Pages 49-60]

  • Soleimani, Hamidreza Modeling and Simulation of a Flexible Spacecraft Solar Panels Deployment Mechanism with Yoke Driven Assembly [Volume 13, Issue 4, 2020, Pages 37-48]

  • Soleimani, Mohamad Design and Fabrication of a dual-polar reflector array antenna for satellite applications [Volume 13, Issue 2, 2020, Pages 99-104]

  • Soleimani, Mohamad Conformal Anti Jamming GPS Antenna with Directive Elements [Volume 13, Issue 3, 2020, Pages 63-68]

  • Soleimaninia, Masume Determination of the Sensitive Volume and Critical Charge for Induction of SEU in Nanometer SRAMs [Volume 16, Issue 2, 2023, Pages 43-54]

  • Soleymani, A. Attitude Control System Design Based on Fluidic Momentum Controllers under Adaptive Sliding Mode [Volume 7, Issue 2, 2014, Pages 63-74]

  • Soltani, Farnoush Study of light spectrums effects on some growth parameters and antioxidant capacity of Anthemis gilanica [Volume 14, Issue 1, 2021, Pages 15-22]

  • Soltani, Mohammadreza Experimental Study of Dynamic Stability for a Entry Capsule in Supersonic Flow [Volume 15, Issue 2, 2022, Pages 71-80]

  • Somayehee, Farshad Determination of the density of scattered spherical data for use in star catalog uniformity [Volume 14, Issue 2, 2021, Pages 103-110]

T

  • Tabatabai, S. Ahmad Military Use and Arms Race in Space from the Perspective of International Law [Volume 15, Issue 4, 2022, Pages 57-70]

  • Tabatabai, S. H. Size Optimization of Space Structures Using Genetic Algorithm and Gradient Methods [Volume 2, Issue 3, 2009, Pages 43-50]

  • Tabataba-Vakili, V Electro-Optical Design of Imaging Payload for a Remote Sensing Satellite [Volume 2, Issue 3, 2009, Pages 57-70]

  • Tabib, Seyyed Mohammad-Jafar Localization of Aerial Robot Based on Fisheye Cameras in a Virtual Lab [Volume 14, Issue 2, 2021, Pages 49-59]

  • Tadayon Mousavi, Samaneh Hot Air Gun Identification by Inverse Heat Transfer [Volume 8, Issue 4, 2016, Pages 29-34]

  • Taefi, M. Space Inertial Navigation System Accuracy Increasing Using Orbit Point Mass Dynamic [Volume 6, Issue 2, 2013, Pages 57-66]

  • Taefi Feijani, Masoud Improvement of the forest canopy density model based on the addition of the FCC index and the average kernel implementation [Volume 14, Issue 2, 2021, Pages 27-36]

  • Taefi Feijani, Masoud Improvement of Forest Canopy Density Model Using Remote Sensing Data Integration [Volume 12, Issue 3, 2019, Pages 31-42]

  • Taei, Hojat Optimal Control of a Tri-axial Spacecraft Simulator Test bed Actuated by Reaction Wheels [Volume 8, Issue 4, 2016, Pages 35-44]

  • Taei, Hojat Monopropellant Propulsion System Design using Multidisciplinary Design Optimization, Sequential Design Method, and Comparing Results [Volume 10, Issue 2, 2017, Pages 53-63]

  • Taei, Hojat Evaluation of Three Design approach of a bipropellant propulsion system including multidisciplinary design optimization, Robust and Optimum-Robust [Volume 12, Issue 1, 2019, Pages 41-53]

  • Taei, Hojat Applying multi-objective optimization approaches to design an optimal controller for orbital docking by consideration of actuators dynamics and comparing results [Volume 13, Issue 2, 2020, Pages 87-96]

  • Taei, Hojat Applying a Novel Comprehensive Preference-based Design (CPD) Approach to Conceptual Design of Space Transportation System [Volume 14, Issue 3, 2021, Pages 39-50]

  • Taei, Hojat Multidisciplinary Design of Bipropellant Propulsion System in Three Methods, Optimal Design, Reliability Based Design and Optimal Reliability Based Design [Volume 14, Issue 4, 2021, Pages 85-98]

  • Taeibi Rahni, Mohammad Drop Behavior on Micro-Structured Superhydrophobic Coating [Volume 15, English Special Issue, 2022, Pages 25-33]

  • Taghavi, A.H. Attitude Control System Design Based on Fluidic Momentum Controllers under Adaptive Sliding Mode [Volume 7, Issue 2, 2014, Pages 63-74]

  • Taghavian, S. H. Governing Equations in Mechanical Analysis of Satellite Carrier Adapter [Volume 5, Issue 1, 2012, Pages 41-50]

  • Taghinezhad, Marzieh Design and implementation of hardware-in-the-loop (HIL) test-bed for spacecraft attitude control [Volume 12, Issue 2, 2019, Pages 55-70]

  • Tahaye Abadi, M. Analysis of Random Positioning System for Simulation of Microgravity [Volume 2, Issue 1, 2009, Pages 25-34]

  • Tahaye Abadi, Mohammad Experimental Analysis of Pyroshock Wave Propagation in Kavoshgar's Payload [Volume 7, Issue 4, 2015, Pages 51-62]

  • Taherbane, M. Evaluation of the Impacts of Orbit Parameters Change on Specifications and Performance of Power Sources of LEO Satellites [Volume 2, Issue 2, 2009, Pages 39-49]

  • Taherbaneh, M. Evaluation of the Effects of Radiation, Irradiance, and Temperature on Solar Cell Electrical Characteristics and Extraction of Maximum Solar Panel Power by MPPT [Volume 1, Issue 1, 2008, Pages 67-80]

  • Taheri, E. Required Velocity Calculation in the Presence Of Atmosphere Effect in C* Matrix [Volume 4, Issue 1, 2011, Pages 69-78]

  • Taheri, R. Design and Fabrication of Laboratory Pilot for OSL Dosimeter System for Space Applications [Volume 6, Issue 3, 2013, Pages 67-73]

  • Taheri Shahraaini, H. Empirical Modeling of Clarity in the Caspian Sea using MERIS Data [Volume 7, Issue 2, 2014, Pages 11-21]

  • Tahmasbi, Hossein Effect of Time Separation between Observations on Angles-only Preliminary Orbit Determination [Volume 8, Issue 2, 2015, Pages 19-26]

  • Tahsini, Amir Mahdi Hot Air Gun Identification by Inverse Heat Transfer [Volume 8, Issue 4, 2016, Pages 29-34]

  • Taji Hervi, Farid Designing Spacecraft Attitude Control Using Model-free Optimal Control Theory [Volume 10, Issue 3, 2017, Pages 41-57]

  • Tajik, H.R. Investigation of Length and Velocity Variation Effects on Unsteady Separation of Parallel Boosters [Volume 7, Issue 2, 2014, Pages 49-61]

  • Talaee, M. R. Satellite Thermal Modeling and Analysis with the Electrical Network Method [Volume 5, Issue 1, 2012, Pages 81-90]

  • Talafi Noghani, Mahmoud Design of an Electromagnetic Band Gap Shield for a Ku-Band VSAT Transmitter Power Amplifier [Volume 14, Issue 1, 2021, Pages 35-41]

  • Talaiee, Hossein GPS Signal Simulation in Intermediate Frequency (IF) [Volume 5, Issue 3, 2012, Pages 33-40]

  • Tavakkoli, A. H. Implementation of Three Axis Attitude Controllers for Evaluation of a Micro-gravity Satellite Simulator [Volume 5, Issue 2, 2012, Pages 59-68]

  • Tavakkoli, Amir Hosein Designing and Evaluation of an Experimental Attitude Determination System Using Sun Sensor and Magnetometer [Volume 5, Issue 4, 2013, Pages 69-78]

  • Tavakoli, A. Constrained Optimization of Launch Vehicle Trajectory Using Spline and Bezier Curves [Volume 2, Issue 2, 2009, Pages 51-60]

  • Tavakoli, Amir Hossein Evaluation of Magnetic Attitude control with Air-Bearing simulator [Volume 9, Issue 2, 2016, Pages 47-60]

  • Tavakoli Sabour, Seyed Mohammad Data Augmentation Investigating in Improving the performance of Deep Learning Model for Building Segmentation using Aerial Images [Volume 15, Issue 3, 2022, Pages 23-32]

  • Tavana, M. Attitude Control of Spacecraft by State Dependent Riccati Equation and Power Series Expansion of Riccati Methods [Volume 7, Issue 4, 2015, Pages 39-49]

  • Tayebi, J. Attitude Stabilization and Manauvring of Agility Nanosatellite with Control Moment Gyros [Volume 7, Issue 2, 2014, Pages 1-9]

  • Tayebi, Javad Attitude Stability Testing of an Agile Satellite Simulator with Single-Gimbal Control-Momentum-Gyros [Volume 5, Issue 4, 2013, Pages 61-68]

  • Tayebi, Javad Designing and Implemntation of PID and Feed back Quaternion Control Strategies for Three Axis Satellite Simulator Equipped With Control Moment Gyros Actiatprs [Volume 9, Issue 1, 2016, Pages 13-23]

  • Tayebi, Sajad Feasibility of Implementig Criminal Jurisdiction in International Space Law [Volume 12, Issue 1, 2019, Pages 1-12]

  • Tayebi, Sobhan Feasibility of Implementig Criminal Jurisdiction in International Space Law [Volume 12, Issue 1, 2019, Pages 1-12]

  • Tayefi, Morteza Design and Dynamic Analysis for Vertical and Horizontal Cylindrical Body in Reentry Flight [Volume 15, Issue 3, 2022, Pages 1-9]

  • Tayefi, Morteza Investigation of MEMS IMU Performance in Sounding Rocket [Volume 12, Issue 4, 2019, Pages 69-77]

  • Tayefi, Morteza Spacecraft Re-entry Control using Cross and Radial Moving-Mass Actuators [(Articles in Press)]

  • Teshneh lab, Mohammad Modeling the Solar Array Design of Remote Sensing Satellites Based on Adaptive Neuro-Fuzzy Inference System [Volume 11, Issue 3, 2018, Pages 1-8]

  • Tirandaz, Mohammad Hossein Optimal Placement of Piezoelectric Sensor/Actuator Patches on Sandwich Panels Considering Debonding Effects [Volume 13, Issue 2, 2020, Pages 37-50]

  • Tivay, M. Studying of Effect of Regularization and Change of Independent Variable on the Solution of Perturbed 2BP [Volume 3, Issue 2, 2011, Pages 53-58]

  • Toloei, Alireza Maximum Likelihood-Based Worst-Case Optimization Design of Hydrazine Propulsion System for aSatellite Orbital Transfer System under Uncertainty [Volume 14, Issue 3, 2021, Pages 1-14]

  • Toloei, Alireza Strap-On Boosters Separation Analysis Using Coupled Simulation of Constraint Dynamics and Time Dependent CFD [Volume 15, English Special Issue, 2022, Pages 35-44]

  • Toloei, Alireza A Method for Determining Design Parameters of Space Umbrella Antenna [Volume 15, Issue 4, 2022, Pages 31-43]

  • Toloei, A. R. Automatic Star Identification Using Triangle Base and Increase Search Speed [Volume 4, Issue 2, 2012, Pages 83-92]

  • Toloui, Alireza Analysis and Improvement of Star Identification Algorithm Based on Singular Value Decomposition for Star Sensor [Volume 16, Issue 4, 2023, Pages 57-70]

  • Torabi, Payman Determining orbital element on Earth Observation Repeat-Ground-Track orbit [Volume 9, Issue 2, 2016, Pages 77-83]

  • Torabi, Seyed Hossein Online Optimal Integrated Guidance and Control Algorithm Design for Launch Vehicle [Volume 8, Issue 2, 2015, Pages 67-78]

  • Torabpoor-Isfahani,, Amir Experimental Study of the Effect of Using Space Sandwich Structures for Protection Against Space Radiation [Volume 15, Issue 2, 2022, Pages 59-69]

V

  • Vafaeesefat, A. Size Optimization of Space Structures Using Genetic Algorithm and Gradient Methods [Volume 2, Issue 3, 2009, Pages 43-50]

  • Vahid D., M. A. Optimal Control of a Tri-axial Spacecraft Simulator Test bed Actuated by Reaction Wheels [Volume 8, Issue 4, 2016, Pages 35-44]

  • Vahidnia, Mohammad Hassan Developing web-based geographical services for temporally vegetation status monitoring using satellite imagery [Volume 13, Issue 4, 2020, Pages 49-58]

  • Valadan Zoej, Mohammad Javad Improvement of Forest Canopy Density Model Using Remote Sensing Data Integration [Volume 12, Issue 3, 2019, Pages 31-42]

  • Vali, Ahmadreza Finite Time Guidance Law to Intercept Desired LOS Angle Using NTSM Control [Volume 11, Issue 2, 2018, Pages 1-10]

  • Vali, Ahmadreza Lyapunov-basedAdaptive SmoothSecond-order Sliding Mode Guidance Law with Proving Finite Time Stability [Volume 11, Issue 2, 2018, Pages 33-39]

  • Vali, Ahmad Reza A New Backstepping Sliding Mode Guidance Law Considering Control Loop Dynamics [Volume 8, Issue 4, 2016, Pages 9-17]

  • Vali, Ahmad Reza Design of an Nonlinear Extended State Observer to Estimate Unmeasurable Information on the Problem of Flying Objects Guidance [Volume 15, Issue 3, 2022, Pages 67-78]

  • ValiMohammad, Afshin Structural Design Modification of a CubeSat Regarding Modal Compatibility for Launching by Vega C Launcher [Volume 16, Issue 4, 2023, Pages 41-56]

  • Varzandian, Gh. A. Optimal Low-Thrust Spacecraft Trajectories Using Time-Domain Finite Element Method [Volume 1, Issue 2, 2008, Pages 43-50]

  • Vaziri Naein Nejad, Javad Effective Parameters of the Aluminum Particles Cyclone Separator in the Effervescent Fuel [Volume 10, Issue 1, 2017, Pages 35-45]

  • Veysi, Hadi Determine the Optimal Orbit for an Earth Observation Satellite Considering the Power [Volume 9, Issue 3, 2016, Pages 27-36]

  • Voosoghi, Behzad Time series modeling of ionosphere total electron content using wavelet neural network and hybrid PSO training algorithm [Volume 13, Issue 3, 2020, Pages 39-50]

  • Voosoghi, Behzad Efficiency of the least squares support vector regression in local modeling of the ionosphere total electron content and comparison with other models [Volume 17, Issue 1, 2024, Pages 21-36]

Y

  • Yadegari Dehkordi, Sajjad Applying a Novel Comprehensive Preference-based Design (CPD) Approach to Conceptual Design of Space Transportation System [Volume 14, Issue 3, 2021, Pages 39-50]

  • Yaghoubi, Kobra A method for determining the optimum parameter of the soft filters to image fusion in the frequency domain [Volume 14, Issue 3, 2021, Pages 23-37]

  • Yahaghi, E. Alterations in Blood Cells Due to Increased Exposure in Space [Volume 6, Issue 2, 2013, Pages 43-48]

  • Ya’ghob-nezhad, Saeedeh Review of a Swirl Double Base Injector Performance by It’s Hot-Fire Test on a Laboratory Liquid Micro Impulse Engine With Single Injector [Volume 9, Issue 1, 2016, Pages 73-89]

  • Yavari, Reza Integrated Guidance and Control Design by Combining Backstepping and Sliding Mode Control Methods [Volume 9, Issue 4, 2017, Pages 39-50]

  • Yazdan, Shabnam Star Catalog Criteria Selection and Mission Catalog Update for a Typical Star Tracker [Volume 5, Issue 4, 2013, Pages 1-8]

  • Yazdani, Shabnam Consideration on Actualizing the Non-Dimensional Star Pattern Recognition Algorithm for a Typical Laboratory Star Tracker [Volume 5, Issue 2, 2012, Pages 15-23]

  • Yazdanian, Masoud Designing and Evaluation of an Experimental Attitude Determination System Using Sun Sensor and Magnetometer [Volume 5, Issue 4, 2013, Pages 69-78]

  • Yeganeh, Hassan Scientometric analysis of published scientific productions in the field of satellite constellations [(Articles in Press)]

  • Yousefzade, Meysam Comparison of Direct and Indirect Georeferencing Methods Using Satellite Linear Array Iimages [Volume 8, Issue 2, 2015, Pages 1-10]

Z

  • Zabihian, Ehsan Complementary Method the Conceptual Design of Space Craft Electrical Power  Subsystem [Volume 8, Issue 3, 2015, Pages 55-63]

  • Zabihian, Ehsan A Software for Establishing Technical Specifications of GEO Communication Satellites [Volume 10, Issue 3, 2017, Pages 1-14]

  • Zabihian, Ehsan GEO Communication Satellite Engineering Design Code [Volume 10, Issue 4, 2018, Pages 41-54]

  • Zabihian, Ehsan GEO satellite station keeping mass design based on data mining [Volume 14, Issue 1, 2021, Pages 23-33]

  • Zabihian, Ehsan Dimensional Direct Simulation Monte Carlo Simulation of Thruster Plumes [Volume 15, Issue 2, 2022, Pages 43-58]

  • Zahednamazi, Mona Analysis and Improvement of Star Identification Algorithm Based on Singular Value Decomposition for Star Sensor [Volume 16, Issue 4, 2023, Pages 57-70]

  • Zahiripour, Seyed Ali Physical Initial Flight Alignment For Stabilized Platform Inertial Navigation system Using State Feedback [Volume 17, Issue 1, 2024, Pages 1-9]

  • Zakeri, Mostafa Integrated Design of Orbital Transfer Block in an Optimized and Multistep Converged Environment [Volume 7, Issue 4, 2015, Pages 23-37]

  • Zakeri, Mostafa Solid Fuel Orbiter Designe in Optimized Space Transfer [Volume 8, Issue 1, 2015, Pages 53-60]

  • Zakeri, Mostafa A New Approach to Engineering Change Management for Spce Projects [Volume 14, Issue 1, 2021, Pages 43-54]

  • Zakiani, Arian Design and Fabrication of Planar Sub-Array for Satellite Data Transmission Directive Conformal Array Antenna [Volume 17, Issue 1, 2024, Pages 73-79]

  • Zamani, Seyyed Ghasem Investigating the Effective Numerical Solution Parameters in Calculating the Roll Damping Coefficient [Volume 10, Issue 3, 2017, Pages 67-75]

  • Zanganeh-nejad, Farzane GPS-RTK Integrated with Micro-Electro Mechanical INS for Precise Application [Volume 5, Issue 3, 2012, Pages 49-57]

  • Zanjirian, Ebrahim Design, Manufacture and Experimental Study of a Hydrogen Peroxide-HTPB Hybrid Rocket Motor [Volume 5, Issue 4, 2013, Pages 19-28]

  • Zardashti, R Flight Path Angle Steering with Lambert Guidance Reference [Volume 2, Issue 2, 2009, Pages 75-79]

  • Zardashti, R. Optimum Transition Orbit Design for Launch Vehicles [Volume 2, Issue 3, 2009, Pages 13-17]

  • Zardashti, R. Ascending Phase Fuzzy Logic Guidance of Satellite Launch Vehicles for Reducing the Adverse Wind Effects [Volume 7, Issue 3, 2014, Pages 75-82]

  • Zarei, P. Attitude nonlinear predictive control of an under actuated spacecraft [Volume 14, Issue 4, 2021, Pages 77-83]

  • Zarourati, Mohammad Design and Implementation of a Balance System for the CubeSat Attitude Determination and Control Tabletop Simulator [Volume 16, Issue 1, 2023, Pages 75-88]

  • Zarrabi, Houman A Review of the Applications of Artificial Intelligence in Improving the Performance of Integrated Space-Air and Ground Networks [Volume 16, Issue 2, 2023, Pages 27-42]

  • Zarrinpour, Vajihe Study of the Effect of the Microgravity on the Expression of Angiogenesis Marker in Endothelial Progenitor Cells [Volume 15, Issue 4, 2022, Pages 89-96]

  • Zarrinpour, Vajiheh Evaluation of Changes in the Expression Level of some Genes Involved in Decompression Sickness in the Pressure Changes [Volume 15, Issue 1, 2022, Pages 41-49]

  • Zayghami, Mohammad Sadegh Introduction to Tadbir satellite Orbit Determination System [Volume 8, Issue 3, 2015, Pages 65-70]

  • Zohoori, Saeed Numerical and Experimental Location Detection of Through Defect in Homogenized Plates using Tomography of Surface Wave Method [Volume 12, Issue 3, 2019, Pages 15-30]