Fixed-Time Fault-Tolerant Optimal Attitude Control of Spacecraft With Performance Constraint via Reinforcement Learning

Engineering

• Performance Constraint 100%
• Attitude Control 100%
• Reinforcement Learning 100%
• Neural Network Weight 50%
• Optimal Controller 50%
• Feedback Control 25%
• Actuator 25%
• Estimation Error 25%
• Optimal Control 25%
• External Disturbance 25%
• Prescribed Performance 25%
• Policy Control 25%
• Persistent Excitation Condition 25%