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]
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
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
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
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
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
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]
