Adaptive Backstepping Control of Spacecraft Rendezvous and Proximity Operations With Input Saturation and Full-State Constraint

• Published in: IEEE transactions on industrial electronics (1982) Vol. 64; no. 1; pp. 480 - 492
• Main Authors: Sun, Liang, Huo, Wei, Jiao, Zongxia
• Format: Journal Article
• Language: English
• Published: New York IEEE 01.01.2017; The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
• Subjects: Adaptive control; Attitude control; Backstepping; Control methods; Control stability; Couplings; Disturbances; Dynamics; Feedback control; Full-state constraint; input saturation; Kinematics; Liapunov functions; model uncertainties; Motion control; Proximity; rendezvous and proximity operations; Saturation; Space rendezvous; Space vehicles; Spacecraft; spacecraft control; Uncertainty
• ISSN: 0278-0046; 1557-9948
• DOI: 10.1109/TIE.2016.2609399

This paper presents a six-degree-of-freedom relative motion control method for autonomous spacecraft rendezvous and proximity operations subject to input saturation, full-state constraint, kinematic coupling, parametric uncertainty, and matched and mismatched disturbances. Relative rotational and relative translational controllers are developed separately based on a unified adaptive backstepping technique. Both element-wise and norm-wise adaptive estimation techniques are used for handling parametric uncertainties, kinematic couplings, and matched and mismatched disturbances, where the bounds of disturbances are unknown. Two auxiliary design systems are employed to deal with input saturation in the relative rotational and relative translational control designs, and the stability of the saturated control solution is verified. Full-state constraint of the relative pose motion is handled by using barrier Lyapunov functions while achieving a satisfactory control performance. All signals in the closed-loop system are guaranteed to be uniformly ultimately bounded, and the relative motion states are all restricted within the known constraints. Compared with the previous control designs of spacecraft rendezvous and proximity operations, the proposed control strategy in this paper can simultaneously deal with input saturation, full-state constraint, kinematic coupling, parametric uncertainty, and matched and mismatched disturbances. Experimental simulation results validate the performance and robustness improvement of the proposed control strategy.