Journal of Space Science and Technology

Journal of Space Science and Technology

Keyword Index
A
  • Attitude control 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]
  • Attitude control 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]
  • Attitude control of satellite 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]
B
  • Bandwidth Designing and Constructing of Inverted F Antennas on a Space Bound Vehicle for Telemetry Transmission [Volume 1, Issue 2, 2008, Pages 57-60]
C
  • Conceptual design Multi-Stage Liquid Propellant Launch Vehicle Conceptual Design, Based on Combinatorial Optimization of Major Design Parameters [Volume 1, Issue 1, 2008, Pages 21-36]
  • Conceptual design software Multi-Stage Liquid Propellant Launch Vehicle Conceptual Design (LVCD) Software, Based on Multi-Parameter Optimization Idea [Volume 1, Issue 2, 2008, Pages 17-25]
D
  • Deployment angle Determination of Deployment Angle for the Optimum Operation of Solar Panels Used in a LEO Satellite [Volume 1, Issue 2, 2008, Pages 1-8]
  • Design optimization Multidisciplinary Design Optimization of a Small Launch Vehicle; a System Sensitivity Analysis Approach [Volume 1, Issue 1, 2008, Pages 47-56]
  • Direct collocation method Optimal Low Thrust Orbit Transfer Using Direct Collocation Method [Volume 1, Issue 2, 2008, Pages 35-42]
E
  • Elasticity satellite Flexible Spacecraft Attitude Control using Hybrid Control Scheme of H∞ and Sliding Mode Control [Volume 1, Issue 2, 2008, Pages 51-56]
  • Environmental test Considerations of Utilizing Telemetry and GPS System in Sounding Rockets [Volume 1, Issue 1, 2008, Pages 81-86]
  • Environment thermal loads Determination of Deployment Angle for the Optimum Operation of Solar Panels Used in a LEO Satellite [Volume 1, Issue 2, 2008, Pages 1-8]
G
  • GPS system Considerations of Utilizing Telemetry and GPS System in Sounding Rockets [Volume 1, Issue 1, 2008, Pages 81-86]
  • Gravity gradient 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]
  • Gravity gradient stabilization 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]
H
  • H∞ control Flexible Spacecraft Attitude Control using Hybrid Control Scheme of H∞ and Sliding Mode Control [Volume 1, Issue 2, 2008, Pages 51-56]
  • HWM Effects of Solar Activities, Drag Coefficient and Atmospheric Wind on Altitude Loss of a LEO Satellite [Volume 1, Issue 1, 2008, Pages 57-66]
I
  • Inverted F Antenna Designing and Constructing of Inverted F Antennas on a Space Bound Vehicle for Telemetry Transmission [Volume 1, Issue 2, 2008, Pages 57-60]
L
  • Launch Vehicle Multi-Stage Liquid Propellant Launch Vehicle Conceptual Design, Based on Combinatorial Optimization of Major Design Parameters [Volume 1, Issue 1, 2008, Pages 21-36]
  • Launch Vehicle Multidisciplinary Design Optimization of a Small Launch Vehicle; a System Sensitivity Analysis Approach [Volume 1, Issue 1, 2008, Pages 47-56]
  • Launch vehicles Multi-Stage Liquid Propellant Launch Vehicle Conceptual Design (LVCD) Software, Based on Multi-Parameter Optimization Idea [Volume 1, Issue 2, 2008, Pages 17-25]
  • LEO 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]
  • Liquid propellant Multi-Stage Liquid Propellant Launch Vehicle Conceptual Design, Based on Combinatorial Optimization of Major Design Parameters [Volume 1, Issue 1, 2008, Pages 21-36]
  • Low Optimal Low-Thrust Spacecraft Trajectories Using Time-Domain Finite Element Method [Volume 1, Issue 2, 2008, Pages 43-50]
  • Low thrust orbit transfer Optimal Low Thrust Orbit Transfer Using Direct Collocation Method [Volume 1, Issue 2, 2008, Pages 35-42]
M
  • Magnetic control 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]
  • Magnetic torquers Satellite Attitude Control by Magnetic Torquers with Variable Magnetic Intensity for Optimization of Power Consumption [Volume 1, Issue 1, 2008, Pages 37-45]
  • Mass regular distribution Multi-Stage Liquid Propellant Launch Vehicle Conceptual Design (LVCD) Software, Based on Multi-Parameter Optimization Idea [Volume 1, Issue 2, 2008, Pages 17-25]
  • Minimum time performance Optimal Low-Thrust Spacecraft Trajectories Using Time-Domain Finite Element Method [Volume 1, Issue 2, 2008, Pages 43-50]
  • Modified equinoctial orbital elements Optimal Low Thrust Orbit Transfer Using Direct Collocation Method [Volume 1, Issue 2, 2008, Pages 35-42]
  • MPPT 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]
  • MSIS Effects of Solar Activities, Drag Coefficient and Atmospheric Wind on Altitude Loss of a LEO Satellite [Volume 1, Issue 1, 2008, Pages 57-66]
  • Multi-stage flight vehicle Development of an Integrated Design Environment for Optimal Ascent Trajectory Planning [Volume 1, Issue 1, 2008, Pages 1-10]
N
  • Nonlinear Programming Optimal Low Thrust Orbit Transfer Using Direct Collocation Method [Volume 1, Issue 2, 2008, Pages 35-42]
  • Nonsingular parameters Effects of Solar Activities, Drag Coefficient and Atmospheric Wind on Altitude Loss of a LEO Satellite [Volume 1, Issue 1, 2008, Pages 57-66]
O
  • Optimal control Optimal Low Thrust Orbit Transfer Using Direct Collocation Method [Volume 1, Issue 2, 2008, Pages 35-42]
  • Optimal design Development of an Integrated Design Environment for Optimal Ascent Trajectory Planning [Volume 1, Issue 1, 2008, Pages 1-10]
  • Optimum mass distribution Multi-Stage Liquid Propellant Launch Vehicle Conceptual Design, Based on Combinatorial Optimization of Major Design Parameters [Volume 1, Issue 1, 2008, Pages 21-36]
P
  • Performance test Considerations of Utilizing Telemetry and GPS System in Sounding Rockets [Volume 1, Issue 1, 2008, Pages 81-86]
  • Perturbation & Observation 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]
  • Photovoltaic system 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]
  • Pitch program Multi-Stage Liquid Propellant Launch Vehicle Conceptual Design, Based on Combinatorial Optimization of Major Design Parameters [Volume 1, Issue 1, 2008, Pages 21-36]
  • Pitch program Multi-Stage Liquid Propellant Launch Vehicle Conceptual Design (LVCD) Software, Based on Multi-Parameter Optimization Idea [Volume 1, Issue 2, 2008, Pages 17-25]
  • Pitch program Development of an Integrated Design Environment for Optimal Ascent Trajectory Planning [Volume 1, Issue 1, 2008, Pages 1-10]
  • Power optimization Satellite Attitude Control by Magnetic Torquers with Variable Magnetic Intensity for Optimization of Power Consumption [Volume 1, Issue 1, 2008, Pages 37-45]
R
  • Radiation 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]
  • Radiation Designing and Constructing of Inverted F Antennas on a Space Bound Vehicle for Telemetry Transmission [Volume 1, Issue 2, 2008, Pages 57-60]
  • Reaction wheels 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]
S
  • Satellite attitude control Satellite Attitude Control by Magnetic Torquers with Variable Magnetic Intensity for Optimization of Power Consumption [Volume 1, Issue 1, 2008, Pages 37-45]
  • Satellite thermal control Deployable solar panels Determination of Deployment Angle for the Optimum Operation of Solar Panels Used in a LEO Satellite [Volume 1, Issue 2, 2008, Pages 1-8]
  • Satellite tool kit Effects of Solar Activities, Drag Coefficient and Atmospheric Wind on Altitude Loss of a LEO Satellite [Volume 1, Issue 1, 2008, Pages 57-66]
  • Saturation 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]
  • Sliding mode Flexible Spacecraft Attitude Control using Hybrid Control Scheme of H∞ and Sliding Mode Control [Volume 1, Issue 2, 2008, Pages 51-56]
  • Slow spinning about yaw axis 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]
  • Solar Cell 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]
  • Sounding rocket Considerations of Utilizing Telemetry and GPS System in Sounding Rockets [Volume 1, Issue 1, 2008, Pages 81-86]
  • Sounding rocket Designing and Constructing of Inverted F Antennas on a Space Bound Vehicle for Telemetry Transmission [Volume 1, Issue 2, 2008, Pages 57-60]
  • Stereo 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]
  • System sensitivity analysis Multidisciplinary Design Optimization of a Small Launch Vehicle; a System Sensitivity Analysis Approach [Volume 1, Issue 1, 2008, Pages 47-56]
T
  • Telemetry system Considerations of Utilizing Telemetry and GPS System in Sounding Rockets [Volume 1, Issue 1, 2008, Pages 81-86]
  • Trajectory Optimization Optimal Low Thrust Orbit Transfer Using Direct Collocation Method [Volume 1, Issue 2, 2008, Pages 35-42]
U
  • Unloading 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]
V
  • Voltage Standing Designing and Constructing of Inverted F Antennas on a Space Bound Vehicle for Telemetry Transmission [Volume 1, Issue 2, 2008, Pages 57-60]
W
  • Wave Ratio Designing and Constructing of Inverted F Antennas on a Space Bound Vehicle for Telemetry Transmission [Volume 1, Issue 2, 2008, Pages 57-60]