基于事件触发采样的无尾翼飞机自适应容错姿态控制

doi:10.12305/j.issn.1001-506X.2024.03.32

Abstract

Abstract:

In view of the attitude tracking control problem of tailless aircraft with limited communication bandwidth, an event-triggered-based adaptive fault-tolerant attitude control method is proposed, in the presence of model uncertainties, external disturbances, and actuator faults. Firstly, a control-oriented attitude control model is established based on the six-degree-of-freedom dynamics and kinematics model of the tailless aircraft. By adopting the event-triggered mechanism, the communication frequency between the controller and the actuator channel is successfully reduced, which relieves the communication burden of the bus and avoids the occurrence of the Zeno phenomenon. Then, the effects of actuator failure and sampling errors caused by the event trigger are successfully compensated by adaptive bounded estimation. Finally, the Lyapunov stability analysis is conducted to demonstrate that the proposed control method ensures the ultimate boundedness of all system signals. Numerical simulation results show that the proposed control method effectively reduces the update frequency of the controller while achieving attitude tracking of the tailless aircraft with respect to control commands.

Key words: tailless aircraft, attitude tracking, event triggered, adaptive control, fault-tolerant control

CLC Number:

V249

Zhilong YU, Yinghui LI, Binbin PEI, Xiaocong DUAN, Zhe ZHANG. Adaptive fault-tolerant attitude control of tailless aircraft based on event-triggered sampling[J]. Systems Engineering and Electronics, 2024, 46(3): 1058-1066.

Figures/Tables 8

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References 12

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控制方法	姿态		角速度		采样次数
控制方法	RMSE	IAE	RMSE	IAE	采样次数
ETM	0.091	1.415	1.158	22.024	2 626
TTM	0.088	1.388	1.107	21.553	28 000
PID	0.161	4.234 3	2.251	67.644 1	28 000

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Adaptive fault-tolerant attitude control of tailless aircraft based on event-triggered sampling

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