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
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