Reducing spacecraft jitter during satellite reorientation maneuvers via solar array dynamics

Keyphrases

• Jitter 100%
• Solar Array 100%
• Reorientation Maneuvers 100%
• Settling Time 66%
• Design Strategy 33%
• Control System 33%
• System Dynamics 33%
• Physical Systems 33%
• Dynamic Model 33%
• Control Strategy 33%
• Optimal Control Problem 33%
• Optimization Methods 33%
• Structural System 33%
• Rigid Body Dynamics 33%
• Pseudo-rigid-body Model 33%
• Control System Design 33%
• Active Dynamics 33%
• Modeling Theory 33%
• Passive Dynamics 33%
• Inertial Properties 33%
• Slewing Maneuver 33%
• Design Formulation 33%
• Jitter Time 33%

Engineering

• Solar Array 100%
• Settling Time 66%
• Control System 33%
• Systems Dynamics 33%
• Rigid Structure 33%
• Control Strategy 33%
• Optimal Control Problem 33%
• Structural System 33%
• Control System Design 33%
• Active Dynamic 33%