Attitude controlDesigning, Testing and Evaluation of Single Gimbal Control Moment Gyro for Microsatellite [Volume 2, Issue 1, 2009, Pages 13-23]
Attitude controlDesign and Manufacturing Steps of a Satellite Reaction Wheel [Volume 2, Issue 2, 2009, Pages 61-68]
B
BatteryEvaluation of the Impacts of Orbit Parameters Change on Specifications and Performance of Power Sources of LEO Satellites [Volume 2, Issue 2, 2009, Pages 39-49]
Bezier and Spline functionConstrained Optimization of Launch Vehicle Trajectory Using Spline and Bezier Curves [Volume 2, Issue 2, 2009, Pages 51-60]
BLDC motorDesign and Manufacturing Steps of a Satellite Reaction Wheel [Volume 2, Issue 2, 2009, Pages 61-68]
BucklingDesign and Fabrication of Protective Corrugated Tunnels for Using in Aerospace Structures [Volume 2, Issue 3, 2009, Pages 27-34]
C
CCD NoisesSatellite Camera CCD Read-out System Design, Based on Noise Optimization with Respect to Satellite Limitations [Volume 2, Issue 3, 2009, Pages 19-26]
CCD Read Out SystemSatellite Camera CCD Read-out System Design, Based on Noise Optimization with Respect to Satellite Limitations [Volume 2, Issue 3, 2009, Pages 19-26]
Cold testDual Base Swirl Injector Design for Increasing Specific Impluse in a Liquid-Fuel Rocket Engine [Volume 2, Issue 1, 2009, Pages 51-57]
D
DebrisDynamic Simulation for Diffusion of Satellite Detached Particles in Various Orbits [Volume 2, Issue 1, 2009, Pages 59-65]
DesignDesign and Fabrication of Protective Corrugated Tunnels for Using in Aerospace Structures [Volume 2, Issue 3, 2009, Pages 27-34]
DESIGN PARAMETERSSatellite Camera CCD Read-out System Design, Based on Noise Optimization with Respect to Satellite Limitations [Volume 2, Issue 3, 2009, Pages 19-26]
DualDual Base Swirl Injector Design for Increasing Specific Impluse in a Liquid-Fuel Rocket Engine [Volume 2, Issue 1, 2009, Pages 51-57]
F
Fault Tree AnalysisModeling and Evaluation of Reliability in Rocket Engine by Fault Tree Analysis [Volume 2, Issue 2, 2009, Pages 69-73]
Finite ElementDesign and Fabrication of Protective Corrugated Tunnels for Using in Aerospace Structures [Volume 2, Issue 3, 2009, Pages 27-34]
Finite ElementSize Optimization of Space Structures Using Genetic Algorithm and Gradient Methods [Volume 2, Issue 3, 2009, Pages 43-50]
Genetic AlgorithmConstrained Optimization of Launch Vehicle Trajectory Using Spline and Bezier Curves [Volume 2, Issue 2, 2009, Pages 51-60]
Genetic AlgorithmSize Optimization of Space Structures Using Genetic Algorithm and Gradient Methods [Volume 2, Issue 3, 2009, Pages 43-50]
K
Kalman FilterDesign of an Attitude Estimation Algorithm for a LEO Satellite Based on Multiple Models Adaptive Method and Comparison with EKF [Volume 2, Issue 2, 2009, Pages 17-26]
L
Launch VehicleA Reliability Growth Model for a Launch Vehicle With its Requirements [Volume 2, Issue 1, 2009, Pages 35-42]
Launch VehicleConstrained Optimization of Launch Vehicle Trajectory Using Spline and Bezier Curves [Volume 2, Issue 2, 2009, Pages 51-60]
LEO OrbitEvaluation of the Impacts of Orbit Parameters Change on Specifications and Performance of Power Sources of LEO Satellites [Volume 2, Issue 2, 2009, Pages 39-49]
LEO satellite cameraSatellite Camera CCD Read-out System Design, Based on Noise Optimization with Respect to Satellite Limitations [Volume 2, Issue 3, 2009, Pages 19-26]
M
MicrogravityAnalysis of Random Positioning System for Simulation of Microgravity [Volume 2, Issue 1, 2009, Pages 25-34]
MicrosatelliteDesigning, Testing and Evaluation of Single Gimbal Control Moment Gyro for Microsatellite [Volume 2, Issue 1, 2009, Pages 13-23]
MTFElectro-Optical Design of Imaging Payload for a Remote Sensing Satellite [Volume 2, Issue 3, 2009, Pages 57-70]
O
Optimal controlClosed-Loop Guidance with Final Velocity Constraint Using Time-Varying Weighting Coefficient for Shaping of Commanded Acceleration [Volume 2, Issue 3, 2009, Pages 1-12]
P
PSFAn Adaptive Method for Star Extraction from Digital Astronomical Images [Volume 2, Issue 2, 2009, Pages 27-38]
R
Reaction wheelDesign and Manufacturing Steps of a Satellite Reaction Wheel [Volume 2, Issue 2, 2009, Pages 61-68]
Reaction wheelSpacecraft Optimal Attitude Control by means of Reaction Wheels [Volume 2, Issue 3, 2009, Pages 35-42]
Reaction wheelsDesign of an Attitude Estimation Algorithm for a LEO Satellite Based on Multiple Models Adaptive Method and Comparison with EKF [Volume 2, Issue 2, 2009, Pages 17-26]
ReliabilityModeling and Evaluation of Reliability in Rocket Engine by Fault Tree Analysis [Volume 2, Issue 2, 2009, Pages 69-73]
S
Satellite LimitationsSatellite Camera CCD Read-out System Design, Based on Noise Optimization with Respect to Satellite Limitations [Volume 2, Issue 3, 2009, Pages 19-26]
SIFTAn Adaptive Method for Star Extraction from Digital Astronomical Images [Volume 2, Issue 2, 2009, Pages 27-38]
Sliding mode controlFlexible Spacecraft Three Axis Attitude Maneuver by Active Vibration Control [Volume 2, Issue 1, 2009, Pages 43-50]
SNRElectro-Optical Design of Imaging Payload for a Remote Sensing Satellite [Volume 2, Issue 3, 2009, Pages 57-70]
StabilityElectro-Optical Design of Imaging Payload for a Remote Sensing Satellite [Volume 2, Issue 3, 2009, Pages 57-70]
T
TestDesign and Fabrication of Protective Corrugated Tunnels for Using in Aerospace Structures [Volume 2, Issue 3, 2009, Pages 27-34]
Trajectory OptimizationConstrained Optimization of Launch Vehicle Trajectory Using Spline and Bezier Curves [Volume 2, Issue 2, 2009, Pages 51-60]