Fault-tolerant Control of Formation Flying Attitude Based on F-16 Fixed-Wing Aircraft
Ying Xin, Wenxuan Liu, Bin Jiang, Xunhong Lv, Hanyu Liang · 2021 CAA Symposium on Fault Detection, Supervision, and Safety for Technical Processes (SAFEPROCESS) · 2021
In this paper, a formation attitude fault-tolerant control strategy based on neighbor information is proposed with actuator faults for F-16 fixed-wing aircraft. To begin with, establish the attitude model and actuator fault model of the F16 fixed-wing aircraft, and then describe a multi-agent systems (MASs) with a ”Leader-Follower” structure. The formation attitude fault-tolerant control of the MASs is divided into formation control and attitude control. The formation controller achieves consistent tracking of multi-agent systems attitude, and the attitude controller performs the attitude tracking control of each fixed-wing aircraft. Finally, simulation results are given to prove the effectiveness of the control method.