Distributed Fault-Tolerant Cooperative Control for Multi-UAVs Under Actuator Fault and Input Saturation

被引:146
作者
Yu, Ziquan [1 ,2 ]
Qu, Yaohong [1 ]
Zhang, Youmin [2 ]
机构
[1] Northwestern Polytech Univ, Sch Automat, Xian 710129, Shaanxi, Peoples R China
[2] Concordia Univ, Dept Mech Ind & Aerosp Engn, Montreal, PQ H3G 1M8, Canada
基金
中国国家自然科学基金;
关键词
Actuators; Fault tolerance; Fault tolerant systems; Decentralized control; Force; Communication networks; Aerodynamics; Actuator fault; distributed control; external disturbance; fault-tolerant cooperative control (FTCC); input saturation; ATTITUDE COORDINATION CONTROL; UNMANNED AERIAL VEHICLES; DYNAMIC SURFACE CONTROL; FLIGHT CONTROL-DESIGN; TRACKING CONTROL; CONTAINMENT CONTROL; SYSTEMS; CONSENSUS;
D O I
10.1109/TCST.2018.2868038
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 investigates a difficult problem of distributed fault-tolerant cooperative control for multiple unmanned aerial vehicles (UAVs) in the presence of actuator faults and input saturation. To eliminate the "explosion of complexity" in the traditional backstepping architecture, the dynamic surface control is utilized to construct the distributed fault-tolerant control scheme. Moreover, by using the disturbance observer technique, actuator faults and external disturbances are estimated as lumped uncertainties. Furthermore, to reduce the adverse influence caused by the control input saturation of UAVs, auxiliary dynamic systems are introduced to regulate the control signals when the input signals are saturated for a long time. The key feature is that the proposed fault-tolerant cooperative controller is designed based on the local information of neighboring UAVs and the factors including actuator faults, input saturation, and external disturbances are simultaneously addressed. It is shown by Lyapunov approach and graph theory that the synchronization tracking stability can be guaranteed and all follower UAVs can track the leader UAV. The effectiveness of the proposed control scheme is further validated by numerical simulation results.
引用
收藏
页码:2417 / 2429
页数:13
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