A
-
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]
-
Ahmadloo, A.
Considerations of Utilizing Telemetry and GPS System in Sounding Rockets [Volume 1, Issue 1, 2008, Pages 81-86]
-
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]
-
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]
-
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]
-
Asadian, Nima
Development of an Integrated Design Environment for Optimal Ascent Trajectory Planning [Volume 1, Issue 1, 2008, Pages 1-10]
B
-
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]
-
Beheshti Boroumand, B.
Considerations of Utilizing Telemetry and GPS System in Sounding Rockets [Volume 1, Issue 1, 2008, Pages 81-86]
-
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]
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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]
E
-
Ebrahimi, M.
Multidisciplinary Design Optimization of a Small Launch Vehicle; a System Sensitivity Analysis Approach [Volume 1, Issue 1, 2008, Pages 47-56]
F
-
Fakhri, M.
Development of an Integrated Design Environment for Optimal Ascent Trajectory Planning [Volume 1, Issue 1, 2008, Pages 1-10]
-
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]
-
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]
-
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]
-
Fazelzadeh, S. A.
Optimal Low-Thrust Spacecraft Trajectories Using Time-Domain Finite Element Method [Volume 1, Issue 2, 2008, Pages 43-50]
G
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Ghafari, A.
Flexible Spacecraft Attitude Control using Hybrid Control Scheme of Hâ and Sliding Mode Control [Volume 1, Issue 2, 2008, Pages 51-56]
-
Ghanbarian, A.
Considerations of Utilizing Telemetry and GPS System in Sounding Rockets [Volume 1, Issue 1, 2008, Pages 81-86]
-
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, 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]
J
-
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]
-
Jamilnia, R.
Optimal Low Thrust Orbit Transfer Using Direct Collocation Method [Volume 1, Issue 2, 2008, Pages 35-42]
-
Jodey, J.
Multidisciplinary Design Optimization of a Small Launch Vehicle; a System Sensitivity Analysis Approach [Volume 1, Issue 1, 2008, Pages 47-56]
K
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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]
-
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]
M
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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]
-
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]
N
-
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]
-
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]
P
-
Pourtakdost, S. Hossein
Development of an Integrated Design Environment for Optimal Ascent Trajectory Planning [Volume 1, Issue 1, 2008, Pages 1-10]
R
-
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]
-
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 Hâ and Sliding Mode Control [Volume 1, Issue 2, 2008, Pages 51-56]
S
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Sadeghi Givi, Z.
Considerations of Utilizing Telemetry and GPS System in Sounding Rockets [Volume 1, Issue 1, 2008, Pages 81-86]
-
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]
-
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]
-
Sayanjali, M.
Flexible Spacecraft Attitude Control using Hybrid Control Scheme of Hâ and Sliding Mode Control [Volume 1, Issue 2, 2008, Pages 51-56]
-
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]
T
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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]
V
-
Varzandian, Gh. A.
Optimal Low-Thrust Spacecraft Trajectories Using Time-Domain Finite Element Method [Volume 1, Issue 2, 2008, Pages 43-50]