Decentralized attitude alignment control of spacecraft within a formation without angular velocity M

Keyphrases

• Control Law 100%
• Angular Velocity 100%
• Auxiliary System 100%
• Without Velocity Measurements 100%
• Attitude Alignment 100%
• Control Problem 50%
• Control Scheme 50%
• Tracking Error 50%
• Rigid Body 50%
• Output Feedback 50%
• Attitude Error 50%
• Communication Link 50%
• Alignment Problem 50%
• Flight Formation 50%
• Relative Attitude 50%
• Coordinated Attitude Control 50%

Engineering

• Control Law 100%
• Angular Velocity ω 100%
• Auxiliary System 100%
• Transients 50%
• Simulation Result 50%
• Control Scheme 50%
• Output Feedback 50%
• Rigid Structure 50%
• Communication Link 50%
• Attitude Control 50%