Event-driven fault-tolerant attitude control of spacecraft with finite-time disturbance observer under input saturation

Engineering

• Finite Time 100%
• Attitude Control 100%
• Spacecraft 100%
• Stabilization Problem 50%
• Comparative Analysis 50%
• Closed Loop 50%
• Model Uncertainty 50%
• External Disturbance 50%
• Control Law 50%
• Loop Stability 50%
• Control Scheme 50%
• Convergence Time 50%
• State Trajectory 50%
• Rate Bound 50%
• Bound State 50%
• Stability Analysis 50%
• Computer Simulation 50%
• Constrainedness 50%
• actuator fault 50%

Computer Science

• Time Disturbance 100%