Multiple rigid-body reorientation using relative motion with constrained final system configuration

Engineering

• Dynamic Condition 100%
• Rigid Structure 100%
• Relative Motion 100%
• Constrainedness 100%
• Control Algorithm 50%
• Geometric Configuration 50%
• Initial State 50%
• Attitude Control 50%
• Desired Target 50%
• Actuator 50%
• Spacecraft 50%

Keyphrases

• System Configuration 100%
• Relative Motion 100%
• Multiple Rigid Bodies 100%
• System Dynamics 50%
• Control Algorithm 50%
• Geometric Configuration 50%
• Control Actuator 50%
• Attitude Control 50%
• System Constraints 50%
• Multibody Spacecraft 50%
• Three-dimensional Mode 50%
• Movable Body 50%