Fault-Tolerant Attitude Control for Rigid Spacecraft Without Angular Velocity Measurements

• Published in: IEEE transactions on cybernetics Vol. 51; no. 3; pp. 1216 - 1229
• Main Authors: Wang, Xianghua, Tan, Chee Pin, Wu, Fen, Wang, Jiandong
• Format: Journal Article
• Language: English
• Published: United States IEEE 01.03.2021; The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
• Subjects: Actuators; Angular velocity; Attitude control; Fault tolerance; Fault-tolerant control (FTC); finite-time observer; Neural networks; neural networks (NNs); Observers; rigid spacecraft attitude control; Sliding mode control; Space vehicles; Spacecraft; Spacecraft attitude control; Twisting; Velocity measurement
• ISSN: 2168-2267; 2168-2275; 2168-2275
• DOI: 10.1109/TCYB.2019.2905427

In this paper, a fault-tolerant control scheme is proposed for the rigid spacecraft attitude control system subject to external disturbances, multiple system uncertainties, and actuator faults. The angular velocity measurement is unavailable, which increases the complexity of the problem. An observer is first designed based on the super-twisting sliding mode method, which can provide accurate estimates of the angular velocity in finite time. Then, an adaptive fault-tolerant controller is proposed based on neural networks using the information from the observer. It is shown that the attitude orientations converge to the desired values exponentially. Finally, a simulation example is utilized to verify the effectiveness of the proposed scheme.