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

被引:183
|
作者
Sun, Liang [1 ]
Huo, Wei [1 ]
Jiao, Zongxia [2 ]
机构
[1] Beihang Univ, Sch Automat Sci & Elect Engn, Res Div 7, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China
[2] Beihang Univ, Sch Automat Sci & Elect Engn, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China
基金
中国国家自然科学基金; 中国博士后科学基金;
关键词
Full-state constraint; input saturation; model uncertainties; rendezvous and proximity operations; spacecraft control; TRAJECTORY TRACKING CONTROL; BARRIER LYAPUNOV FUNCTIONS; SLIDING MODE CONTROL; NONLINEAR-SYSTEMS; FEEDBACK-CONTROL; RELATIVE MOTION; ROBUST-CONTROL; POSE TRACKING; ATTITUDE; VELOCITY;
D O I
10.1109/TIE.2016.2609399
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
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.
引用
收藏
页码:480 / 492
页数:13
相关论文
共 50 条
  • [31] Potential function based robust safety control for spacecraft rendezvous and proximity operations under path constraint
    Li, Qi
    Zhang, Bo
    Yuan, Jianping
    Wang, Huan
    ADVANCES IN SPACE RESEARCH, 2018, 62 (09) : 2586 - 2598
  • [32] Adaptive Neural Tracking Control of Full-state Constrained Nonstrict-feedback Time-delay Systems with Input Saturation
    Xin Liu
    Chuang Gao
    Huanqing Wang
    Libing Wu
    Yonghui Yang
    International Journal of Control, Automation and Systems, 2020, 18 : 2048 - 2060
  • [33] Finite-time attitude control for fixed-wing UAVs with full-state constraints and input saturation
    Jiao, Dexin
    Wang, Yani
    Chen, Yaowen
    Lu, Weifan
    Zou, An-Min
    Yang, Xuerong
    JOURNAL OF THE FRANKLIN INSTITUTE, 2025, 362 (04)
  • [34] Adaptive Fuzzy Control for High-Order Nonlinear Time-Delay Systems With Full-State Constraints and Input Saturation
    Wu, You
    Xie, Xue-Jun
    IEEE TRANSACTIONS ON FUZZY SYSTEMS, 2020, 28 (08) : 1652 - 1663
  • [35] Adaptive robust fault-tolerant control scheme for spacecraft proximity operations under external disturbances and input saturation
    Yu Wang
    Kang Liu
    Haibo Ji
    Nonlinear Dynamics, 2022, 108 : 207 - 222
  • [36] Characteristic Model Based Robust H∞ Control for Spacecraft Rendezvous and Proximity Operations
    Lu, Yao
    Jia, Yingmin
    2021 PROCEEDINGS OF THE 40TH CHINESE CONTROL CONFERENCE (CCC), 2021, : 7683 - 7688
  • [37] Adaptive Neural Tracking Control of Full-state Constrained Nonstrict-feedback Time-delay Systems with Input Saturation
    Liu, Xin
    Gao, Chuang
    Wang, Huanqing
    Wu, Libing
    Yang, Yonghui
    INTERNATIONAL JOURNAL OF CONTROL AUTOMATION AND SYSTEMS, 2020, 18 (08) : 2048 - 2060
  • [38] Backstepping control for attitude tracking of the spacecraft under input saturation
    Guo, Yong
    Guo, Jin-hua
    Song, Shen-min
    ACTA ASTRONAUTICA, 2017, 138 : 318 - 325
  • [39] Disturbance observer based control for spacecraft proximity operations with path constraint
    Li, Qi
    Yuan, Jianping
    Zhang, Bo
    Wang, Huan
    AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 79 : 154 - 163
  • [40] Robust adaptive control for spacecraft final proximity maneuvers with safety constraint and input quantization
    Li, Qi
    Sun, Chong
    Song, Shuo
    Gou, Qiuxiong
    Niu, Zhiqi
    ISA TRANSACTIONS, 2021, 111 : 35 - 46