Distributed adaptive attitude tracking of multiple spacecraft with a leader of nonzero input

Engineering

• Adaptive Controller 100%
• Adaptive Gain 50%
• Angular Velocity ω 50%
• Communication Graph 50%
• Control Input 50%
• Spanning Tree 50%

Computer Science

• Adaptive Control Systems 100%
• Angular Velocity 50%
• Communication Graph 50%
• Spanning Tree 50%
• Tracking Error 50%