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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

  • Accommodation 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]

  • Adaptive thresholds 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]

  • Aeroheatin 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]

  • Antenna miniaturization 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]

  • Approximat boundary 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]

  • Astrounats 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]

  • AT90CAN Total Ionizing Dose Test on AT90CAN128 MicroController [Volume 6, Issue 4, 2013, Pages 63-67]

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

B

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

C

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

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

  • Communication satellite Design and Aanalysis of Sandwich Panels as a Support Structure of Solar Cells for a GEO Communications Satellite [Volume 6, Issue 4, 2013, Pages 13-22]

  • Cosmic ray reduction 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]

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

  • COTS Total Ionizing Dose Test on AT90CAN128 MicroController [Volume 6, Issue 4, 2013, Pages 63-67]

  • Cut Modeling of Shutdown Process in Liquid Propellant Rocket Engines [Volume 6, Issue 4, 2013, Pages 1-11]

D

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

  • Design of round trip Design of Round Trip Trajectories to Lunar L1 [Volume 6, Issue 3, 2013, Pages 49-54]

  • Differential flatness Explicit Flatness-Based Guidance in Reentry Phase [Volume 6, Issue 4, 2013, Pages 29-36]

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

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

  • Displacement of atoms 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]

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

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

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

E

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

  • Encounter plane 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]

  • Explicitguidance Explicit Flatness-Based Guidance in Reentry Phase [Volume 6, Issue 4, 2013, Pages 29-36]

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

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

F

  • Fault Isolation 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]

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

  • Finite Element Design and Aanalysis of Sandwich Panels as a Support Structure of Solar Cells for a GEO Communications Satellite [Volume 6, Issue 4, 2013, Pages 13-22]

  • Flight simulation Developing a Multi-Objective Guidance Scenario for the Entry to the Earth’s Atmosphere [Volume 6, Issue 4, 2013, Pages 53-62]

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

G

  • Gaussian density function 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]

  • GEANT4 Sensitive Volume Modeling in Calculation of Space Radiation-Induced SEU Cross Section [Volume 6, Issue 4, 2013, Pages 23-28]

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

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

  • Ground station 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]

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

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

H

  • High Impedance surfaces 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]

  • Honeycomb Design and Aanalysis of Sandwich Panels as a Support Structure of Solar Cells for a GEO Communications Satellite [Volume 6, Issue 4, 2013, Pages 13-22]

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

  • Hypergravitye The Study of Hypergravity and Flight Stress on Different Cell Lines Function in Sounding Rocket [Volume 6, Issue 4, 2013, Pages 37-42]

  • Hypersonic Flow 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]

I

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

  • Imaging A New Approach to Design an Optimum Launch Window for a Sample Micro-Satellite [Volume 6, Issue 4, 2013, Pages 43-52]

  • Integral sliding mode control Robust Control of Spacecraft Formation Flying Using Optimal Sliding Mode [Volume 6, Issue 1, 2013, Pages 69-75]

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

  • Integred matrix method 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]

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

  • Interval observer 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]

  • Inverse dynamics Explicit Flatness-Based Guidance in Reentry Phase [Volume 6, Issue 4, 2013, Pages 29-36]

  • Ionization 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]

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

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

K

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

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

L

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

  • Launch window A New Approach to Design an Optimum Launch Window for a Sample Micro-Satellite [Volume 6, Issue 4, 2013, Pages 43-52]

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

  • Liquid fuel engine Dynamics Simulation of Pressurizing in Propulsion System Configuration [Volume 6, Issue 3, 2013, Pages 1-13]

  • Liquid propellant rocket engine Modeling of Shutdown Process in Liquid Propellant Rocket Engines [Volume 6, Issue 4, 2013, Pages 1-11]

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

M

  • Magnetic conductors 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]

  • Maximum collision probability 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]

  • Micro A New Approach to Design an Optimum Launch Window for a Sample Micro-Satellite [Volume 6, Issue 4, 2013, Pages 43-52]

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

  • Modeling Modeling of Shutdown Process in Liquid Propellant Rocket Engines [Volume 6, Issue 4, 2013, Pages 1-11]

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

  • Multiple shooting method Design of Round Trip Trajectories to Lunar L1 [Volume 6, Issue 3, 2013, Pages 49-54]

N

  • Navid satellite 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]

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

  • Non 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]

O

  • Optimal sliding mode control Robust Control of Spacecraft Formation Flying Using Optimal Sliding Mode [Volume 6, Issue 1, 2013, Pages 69-75]

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

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

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

  • Outer space law 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]

  • Outer space treary 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]

P

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

  • Perturbation factors Developing a New Explicit Guidance Method for the Trajectory Correction of Sub-Orbital Modules [Volume 6, Issue 3, 2013, Pages 15-26]

  • Positional covariance ellipsoid 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]

  • Position determination 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]

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

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

  • Power Generation A New Approach to Design an Optimum Launch Window for a Sample Micro-Satellite [Volume 6, Issue 4, 2013, Pages 43-52]

  • Propagation model 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]

Q

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

R

  • Radiation damage 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]

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

  • RDA algorithm SAR Imaging Systems Performance Modeling [Volume 6, Issue 1, 2013, Pages 47-56]

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

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

  • Reaction wheels 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]

  • Reconfiguration 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]

  • Reentry Explicit Flatness-Based Guidance in Reentry Phase [Volume 6, Issue 4, 2013, Pages 29-36]

  • Reentry Developing a Multi-Objective Guidance Scenario for the Entry to the Earth’s Atmosphere [Volume 6, Issue 4, 2013, Pages 53-62]

  • Relative motion in circular orbit Robust Control of Spacecraft Formation Flying Using Optimal Sliding Mode [Volume 6, Issue 1, 2013, Pages 69-75]

  • Remote Sensing A New Approach to Design an Optimum Launch Window for a Sample Micro-Satellite [Volume 6, Issue 4, 2013, Pages 43-52]

  • Return and rescue agreement 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]

S

  • Sandwich Panel Design and Aanalysis of Sandwich Panels as a Support Structure of Solar Cells for a GEO Communications Satellite [Volume 6, Issue 4, 2013, Pages 13-22]

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

  • Semiconductor component 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]

  • Sensitive volume Sensitive Volume Modeling in Calculation of Space Radiation-Induced SEU Cross Section [Volume 6, Issue 4, 2013, Pages 23-28]

  • Sensitiviy functions Developing a Multi-Objective Guidance Scenario for the Entry to the Earth’s Atmosphere [Volume 6, Issue 4, 2013, Pages 53-62]

  • SEU damage Sensitive Volume Modeling in Calculation of Space Radiation-Induced SEU Cross Section [Volume 6, Issue 4, 2013, Pages 23-28]

  • SGP4 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]

  • Shutdown Modeling of Shutdown Process in Liquid Propellant Rocket Engines [Volume 6, Issue 4, 2013, Pages 1-11]

  • Signal space to image spaceMapping SAR Imaging Systems Performance Modeling [Volume 6, Issue 1, 2013, Pages 47-56]

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

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

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

  • Slow positron beam system Positron Annihilation Spectroscopy in Materials and Technical Details of Measurement Systems [Volume 6, Issue 2, 2013, Pages 1-10]

  • Solar Cell Design and Aanalysis of Sandwich Panels as a Support Structure of Solar Cells for a GEO Communications Satellite [Volume 6, Issue 4, 2013, Pages 13-22]

  • Sounding rocket The Study of Hypergravity and Flight Stress on Different Cell Lines Function in Sounding Rocket [Volume 6, Issue 4, 2013, Pages 37-42]

  • Space debris 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]

  • Space propulsion system Dynamics Simulation of Pressurizing in Propulsion System Configuration [Volume 6, Issue 3, 2013, Pages 1-13]

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

  • Space Tourism 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]

  • SRAM Sensitive Volume Modeling in Calculation of Space Radiation-Induced SEU Cross Section [Volume 6, Issue 4, 2013, Pages 23-28]

  • Stable and unstable Manifold Design of Round Trip Trajectories to Lunar L1 [Volume 6, Issue 3, 2013, Pages 49-54]

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

  • Stress The Study of Hypergravity and Flight Stress on Different Cell Lines Function in Sounding Rocket [Volume 6, Issue 4, 2013, Pages 37-42]

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

T

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

  • Three body problem Design of Round Trip Trajectories to Lunar L1 [Volume 6, Issue 3, 2013, Pages 49-54]

  • TID Test Total Ionizing Dose Test on AT90CAN128 MicroController [Volume 6, Issue 4, 2013, Pages 63-67]

  • TLE 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]

  • Trajectory shaping Developing a Multi-Objective Guidance Scenario for the Entry to the Earth’s Atmosphere [Volume 6, Issue 4, 2013, Pages 53-62]

  • TRIM 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]

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

  • Two line element set 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]

V

  • Virtual displacement Developing a New Explicit Guidance Method for the Trajectory Correction of Sub-Orbital Modules [Volume 6, Issue 3, 2013, Pages 15-26]