Fully Actuated System Approach Based Prescribed-Time Fault-Tolerant Formation Control for Unmanned Helicopters Under Fixed and Switching Topologies

被引:0
|
作者
Lu, Yuan [1 ]
Zhang, Ke [1 ,2 ]
Jiang, Bin [1 ,2 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Automation Engn, Nanjing 211106, Peoples R China
[2] Natl Key Lab Helicopter Aeromech, Nanjing 210016, Peoples R China
关键词
Topology; Switches; Control systems; Formation control; Actuators; Fault tolerant systems; Fault tolerance; Unmanned helicopters; fully actuated system approach; prescribed-time control; actuator faults; switching communication topologies; CONTAINMENT CONTROL; TRACKING CONTROL; FUZZY-SYSTEMS;
D O I
10.1109/TCSI.2024.3399779
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
The fault-tolerant formation control problem for unmanned helicopters (UHs) with actuator faults under fixed and switching communication topologies is investigated in this paper. Firstly, the high-order fully actuated system model of the 6-DOF UH is established, which is divided into the position outer-loop subsystem and the attitude inner-loop subsystem. Secondly, a prescribed-time disturbance observer is constructed to rapidly and accurately estimate the composite disturbances composed of external disturbances and actuator faults. Then, with the aid of the fully actuated system approach, the formation fault-tolerant controller and attitude tracking fault-tolerant controller are designed for the inner and outer loops respectively, which can guarantee the prescribed-time stability of multiple UHs under fixed and switching topologies. Finally, the simulation results are provided to demonstrate the effectiveness of the proposed control strategy.
引用
收藏
页码:5249 / 5260
页数:12
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