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A B C D E F G H I J K L M N O P Q R S T U V W X Y Z ALL

A

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

  • 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]

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

  • Akhlomadi, Mehdi Reza Nonlinear Optimal Control of Space Docking and Rendezvous Problem [Volume 8, Issue 3, 2015]

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

  • 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]

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

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

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

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

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

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

B

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

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

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

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

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

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

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

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

D

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

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

E

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

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

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

F

  • 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]

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

  • Fathi, Mohsen Design a μ-Controller To Control Attitude of a Flexible Microsatellite [Volume 8, Issue 1, 2015]

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

G

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

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

H

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

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

I

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

K

  • 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]

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

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

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

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

  • Kashaninia, Abdol Reza Design a μ-Controller To Control Attitude of a Flexible Microsatellite [Volume 8, Issue 1, 2015]

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

L

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

M

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

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

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

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

  • Mohsenipour, Reza Design a μ-Controller To Control Attitude of a Flexible Microsatellite [Volume 8, Issue 1, 2015]

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

N

  • Nasirian, M. New Satellite Automatic Tracking by Doppler [Volume 8, Issue 2, 2015]

  • Nasirian, Mehrzad Design a μ-Controller To Control Attitude of a Flexible Microsatellite [Volume 8, Issue 1, 2015]

  • Navabi, Mohammad Nonlinear Optimal Control of Space Docking and Rendezvous Problem [Volume 8, Issue 3, 2015]

  • Nosrat Elahi, Mehran Solid Fuel Orbiter Designe in Optimized Space Transfer [Volume 8, Issue 1, 2015]

P

  • Pariz, Naser Nonlinear Dynamic Inversion Fault Tolerant Control for Spacecraft    [Volume 8, Issue 2, 2015]

R

  • Refan, Mohammad Hossein Improving DGPS Accuracy Using Predictions of Reference Position Components Error Factors [Volume 8, Issue 2, 2015]

  • R. Najafi, Hamed Evaluation of Effective Emissivity of a Multilayer Insulation Blanket Using Test [Volume 8, Issue 1, 2015]

  • Roshanian, Jafar Combining Gradient and Evolutionary Algorithms for Improving Collaborative Optimization Performance [Volume 8, Issue 2, 2015]

  • Roshanian, Jafar Online Optimal Integrated Guidance and Control Algorithm Design for Launch Vehicle [Volume 8, Issue 2, 2015]

S

  • Saghari, Asad Complementary Method the Conceptual Design of Space Craft Electrical Power  Subsystem [Volume 8, Issue 3, 2015]

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

  • Shafiei, Mohammad Hossein New Approach in Guidance Law Design Based on Finite-Time Partial Stability Theorem [Volume 8, Issue 1, 2015]

  • 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]

  • 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]

  • Sharifi, Ali Reza Comparison of Direct and Indirect Georeferencing Methods Using Satellite Linear Array Iimages [Volume 8, Issue 2, 2015]

T

  • Tadayon Mousavi, Samaneh Hot Air Gun Identification by Inverse Heat Transfer [Volume 8, Issue 4, 2016, Pages 29-34]

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

  • Tahmasbi, Hossein Effect of Time Separation between Observations on Angles-only Preliminary Orbit Determination [Volume 8, Issue 2, 2015]

  • Tahsini, Amir Mahdi Hot Air Gun Identification by Inverse Heat Transfer [Volume 8, Issue 4, 2016, Pages 29-34]

  • Torabi, Seyed Hossein Online Optimal Integrated Guidance and Control Algorithm Design for Launch Vehicle [Volume 8, Issue 2, 2015]

V

  • 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]

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

Y

  • Yousefzade, Meysam Comparison of Direct and Indirect Georeferencing Methods Using Satellite Linear Array Iimages [Volume 8, Issue 2, 2015]

Z

  • Zabihian, Ehsan Complementary Method the Conceptual Design of Space Craft Electrical Power  Subsystem [Volume 8, Issue 3, 2015]

  • Zakeri, Mostafa Solid Fuel Orbiter Designe in Optimized Space Transfer [Volume 8, Issue 1, 2015]

  • Zayghami, Mohammad Sadegh Introduction to Tadbir satellite Orbit Determination System [Volume 8, Issue 3, 2015]