Adaptive neural fault-tolerant control for output-constrained attitude tracking of unmanned space vehicles

被引:5
|
作者
Yao, Qijia [1 ]
Jahanshahi, Hadi [2 ]
Golestani, Mehdi [3 ]
机构
[1] Beijing Inst Technol, Sch Aerosp Engn, 5 South Zhongguancun St, Beijing 100081, Peoples R China
[2] Univ Manitoba, Dept Mech Engn, Winnipeg, MB, Canada
[3] Iran Univ Sci & Technol, Dept Elect Engn, Tehran, Iran
关键词
Attitude tracking control; unmanned space vehicle; adaptive neural control; fault-tolerant control; output constraints; SLIDING-MODE CONTROL; TRAJECTORY TRACKING; NONLINEAR-SYSTEMS; PRESCRIBED PERFORMANCE; FLEXIBLE SPACECRAFT; RIGID SPACECRAFT; CONTROL DESIGN; QUADROTOR UAV; STABILIZATION; SATELLITE;
D O I
10.1177/01423312221135213
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
The challenging problem of attitude tracking control for unmanned space vehicles (USVs) subject to actuator faults and output constraints is addressed in this study. A novel adaptive neural fault-tolerant controller is proposed by integrating the neural networks (NNs) and barrier Lyapunov function (BLF) with the backstepping technique. Two NNs are adopted to approximate the uncertain nonlinear terms caused by unknown attitude dynamics and actuator faults, respectively. Moreover, the BLF is introduced to tackle the output constraints. It is strictly proved that all the closed-loop error signals are uniformly ultimately bounded under the proposed controller. Totally, the proposed adaptive neural fault-tolerant controller has the following two distinctive features. (1) The proposed controller is model-free and can still be applicable even when the USV attitude dynamic model is completely unknown in advance. (2) The proposed controller can guarantee the attitude tracking error always within the predefined output constraints even in the presence of actuator faults and thus ensuring safety. Finally, the excellent tracking performance of the proposed controller is verified through numerical simulations and comparisons.
引用
收藏
页码:1229 / 1244
页数:16
相关论文
共 50 条
  • [41] Fault-tolerant model predictive control for unmanned surface vehicles
    Asfihani, Tahiyatul
    Syafi'i, Ahmad Maulana
    Hasan, Agus
    SYSTEMS SCIENCE & CONTROL ENGINEERING, 2025, 13 (01)
  • [42] Fixed-time neural adaptive fault-tolerant control for space manipulator under output constraints
    Yao, Qijia
    ACTA ASTRONAUTICA, 2023, 203 : 483 - 494
  • [43] Fault-tolerant control via integral sliding mode output feedback for unmanned marine vehicles
    Hao, Li-Ying
    Zhang, Yu-Qing
    Li, Hui
    APPLIED MATHEMATICS AND COMPUTATION, 2021, 401
  • [44] L1 neural network adaptive fault-tolerant controller for unmanned aerial vehicle attitude control system
    Zhou, Yan
    Liu, Huiying
    Guo, Huijuan
    Li, Jing
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2021, 235 (13) : 1779 - 1790
  • [45] Adaptive fuzzy fault-tolerant attitude control of spacecraft
    Zou, An-Min
    Kumar, Krishna Dev
    CONTROL ENGINEERING PRACTICE, 2011, 19 (01) : 10 - 21
  • [46] Robust constrained fault-tolerant attitude control for flexible spacecraft
    Long, Haihui
    Zhao, Jiankang
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2018, 232 (16) : 3011 - 3023
  • [47] Adaptive Sliding Mode Fault-tolerant Control for Attitude Tracking of Spacecraft With Actuator Faults
    Yu Xuan Yang
    Ming Chen
    Kai Xiang Peng
    Man Yu
    International Journal of Control, Automation and Systems, 2023, 21 : 2587 - 2594
  • [48] Adaptive Fault-Tolerant Control for Attitude Tracking of Flexible Spacecraft With Limited Data Transmission
    Liu, Qiuhong
    Liu, Ming
    Yu, Jinyong
    IEEE TRANSACTIONS ON SYSTEMS MAN CYBERNETICS-SYSTEMS, 2021, 51 (07): : 4400 - 4408
  • [49] Adaptive Fault-Tolerant Attitude Tracking Control for Flexible Spacecraft With Guaranteed Performance Bounds
    Xiao, Yan
    de Ruiter, Anton
    Ye, Dong
    Sun, Zhaowei
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2022, 58 (03) : 1922 - 1940
  • [50] Adaptive Sliding Mode Fault-tolerant Control for Attitude Tracking of Spacecraft With Actuator Faults
    Yang, Yu Xuan
    Chen, Ming
    Peng, Kai Xiang
    Yu, Man
    INTERNATIONAL JOURNAL OF CONTROL AUTOMATION AND SYSTEMS, 2023, 21 (08) : 2587 - 2594