Dynamic surface control for satellite attitude of the chained three-body tethered system during deployment

Engineering

• Actuator 33%
• Angular Velocity ω 33%
• Attitude Control 33%
• Auxiliary System 33%
• Closed System 33%
• Control Input 33%
• Control Scheme 33%
• Control Strategy 33%
• Control Surface 100%
• Controller Design 33%
• Convergence Time 33%
• Error Compensation 33%
• Extended State Observer 33%
• Inertia Tensor 33%
• Input Constraint 33%
• Limitations 33%