无人机电制动系统的级联快速终端滑模控制

Q3 Engineering
Yuren Li, Hongyu Zhang, Liang Tian, Yufan Zhang, Y. Rao, Yuntong Li, Bo Liang
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引用次数: 0

摘要

无人机防滑制动系统具有高阶非线性、强耦合、参数时变等特点,会严重影响无人机的滑行性能。本文提出了一种用于无人机电制动系统的级联快速终端滑模控制方法,该方法可以准确跟踪最优滑差率,确保制动系统的稳定性。首先,建立了无人机电制动系统模型,摆脱了对地面束缚系数拟合公式的依赖。其次,结合逆变控制的概念,设计了级联快速终端滑模控制器,以实现对滑移率和参考制动力的精确跟踪。利用李雅普诺夫稳定性理论证明了控制器的稳定性。最后,仿真结果验证了所提控制策略的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Cascaded fast terminal sliding mode control for UAV electric braking system
The anti-skid braking system of unmanned aerial vehicle has the characteristics of high-order nonlinearity, strong coupling, and time-varying parameters, which will seriously affect the taxiing performance of the unmanned aerial vehicle. This paper proposed a cascaded fast terminal sliding mode control method for unmanned aerial vehicle electric braking system, which can accurately track the optimal slip rate and ensure the stability of the braking system. First, the electric braking system model of unmanned aerial vehicle is established, which gets rid of the reliance on the ground binding coefficient fitting formulas. Second, combined with the concept of the inversion control, the cascaded fast terminal sliding mode controller is designed to achieve the accurate tracking of the slip rate and the reference braking force. The stability of the controller is proved by the Lyapunov stability theory. Finally, the effectiveness of the proposed control strategy is verified by simulation results.
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来源期刊
西北工业大学学报
西北工业大学学报 Engineering-Engineering (all)
CiteScore
1.30
自引率
0.00%
发文量
6201
审稿时长
12 weeks
期刊介绍:
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