Distributed Finite-Time Fault-Tolerant Containment Control for Multiple Unmanned Aerial Vehicles

被引:168
作者
Yu, Ziquan [1 ,2 ,3 ]
Liu, Zhixiang [3 ]
Zhang, Youmin [3 ]
Qu, Yaohong [2 ]
Su, Chun-Yi [3 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 211106, Peoples R China
[2] Northwestern Polytech Univ, Sch Automat, Xian 710129, Peoples R China
[3] Concordia Univ, Dept Mech Ind & Aerosp Engn, Montreal, PQ H3G 1M8, Canada
基金
中国国家自然科学基金; 加拿大自然科学与工程研究理事会;
关键词
Fault tolerance; Fault tolerant systems; Actuators; Aerodynamics; Unmanned aerial vehicles; Artificial neural networks; Convergence; Distributed fault-tolerant containment control; finite-time control; input saturation; neural networks (NNs); unmanned aerial vehicles (UAVs); NEURAL-NETWORK CONTROL; FLIGHT CONTROL-DESIGN; NONLINEAR-SYSTEMS; TRACKING CONTROL; COOPERATIVE CONTROL; FEEDBACK SYSTEMS; ADAPTIVE-CONTROL; UAVS; STABILIZATION; TECHNOLOGIES;
D O I
10.1109/TNNLS.2019.2927887
中图分类号
TP18 [人工智能理论];
学科分类号
081104 ; 0812 ; 0835 ; 1405 ;
摘要
This paper investigates the distributed finite-time fault-tolerant containment control problem for multiple unmanned aerial vehicles (multi-UAVs) in the presence of actuator faults and input saturation. The distributed finite-time sliding-mode observer (SMO) is first developed to estimate the reference for each follower UAV. Then, based on the estimated knowledge, the distributed finite-time fault-tolerant controller is recursively designed to guide all follower UAVs into the convex hull spanned by the trajectories of leader UAVs with the help of a new set of error variables. Moreover, the unknown nonlinearities inherent in the multi-UAVs system, computational burden, and input saturation are simultaneously handled by utilizing neural network (NN), minimum parameter learning of NN (MPLNN), first-order sliding-mode differentiator (FOSMD) techniques, and a group of auxiliary systems. Furthermore, the graph theory and Lyapunov stability analysis methods are adopted to guarantee that all follower UAVs can converge to the convex hull spanned by the leader UAVs even in the event of actuator faults. Finally, extensive comparative simulations have been conducted to demonstrate the effectiveness of the proposed control scheme.
引用
收藏
页码:2077 / 2091
页数:15
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