Code - Active fault-tolerant system design for a rigid spacecraft in the presence of actuator faults and saturation constraints.

Please refer to the reference:

Q. Shen, C. F. Yue, C. H. Goh and D. W. Wang, “Active Fault-Tolerant Control System Design for Spacecraft Attitude Maneuvers with Actuator Saturation and Faults,” IEEE Transactions on Industrial Electronics, 66(5), pp. 3763-3772, 2019.

List of capabilities:

• Detect actuator faults in rigid-body attitude control systems
• Estimate combined actuator faults by using a disturbance observer
• Design an adaptive controller to compensate actuator fault effects taking into account actuator saturation constraints.