Performance Attitude Tracking Control for Spacecraft during Target Damping by Electromagnetic Eddy Current

Engineering

• Sliding-Mode Controller 100%
• Performance Function 100%
• Tasks 50%
• External Disturbance 50%
• Finite Time 50%
• Control Law 50%
• Cooperative 50%
• Singularities 50%
• Convergence Performance 50%
• State Response 50%
• Prescribed Performance 50%
• Error Value 50%
• Gain Matrix 50%