Optimal reorientation of a multibody spacecraft through joint motion using averaging theory

Keyphrases

• Joint Motion 100%
• Averaging Theory 100%
• Multibody Spacecraft 100%
• Angular Momentum 50%
• Control Algorithm 50%
• Four-link 50%
• Secular Variation 50%
• Periodic Actuation 50%
• Multibody Systems 50%
• Analytic Control 50%
• Control Profile 50%
• Optimal Control Theory 50%
• Control Effort 50%
• Controlled Choice 50%
• Control Vector 50%
• Secular Motion 50%

Engineering

• Joints (Structural Components) 100%
• Actuation 50%
• Angular Momentum 50%
• Control Algorithm 50%
• Profile Control 50%
• Optimal Control 50%
• Multibody System 50%
• Control Vector 50%