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吸气式高超声速飞行器预设反演鲁棒控制

  • 王鹏飞 1 ,
  • 罗畅 2 ,
  • 刘承君 1 ,
  • 张峰 1 ,
  • 章华 1
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  • 1 陆军炮兵防空兵学院,合肥 230031
  • 2 78092部队,成都 610000

王鹏飞(1988—),男,河南开封人,讲师,博士,研究方向:非线性控制。

收稿日期: 2020-05-16

  网络出版日期: 2025-02-25

基金资助

安徽省自然科学基金(2008085QF332)

Back-stepping Robust Control for Air-breathing Hypersonic Vehicles with Prescribed Performance

  • WANG Pengfei 1 ,
  • LUO Chang 2 ,
  • LIU Chengjun 1 ,
  • ZHANG Feng 1 ,
  • ZHANG Hua 1
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  • 1 Army Academy of Artillery and Air Defence,Hefei 230031,China
  • 2 No.78092 Unit,Chengdu 610000,China

Received date: 2020-05-16

  Online published: 2025-02-25

摘要

针对吸气式高超声速飞行器动力学模型,设计一种基于预设性能的反演鲁棒控制器。在反演控制的设计框架下,基于预设性能函数对跟踪误差进行转换实现对收敛速度、超调量的约束。为解决反演控制鲁棒性能较弱的问题,基于改进的反正切微分器构造了一种新型干扰观测器,对模型中的不确定项进行估计。仿真实验表明,该方法能够较好的实现对控制系统瞬态性能的约束。

本文引用格式

王鹏飞 , 罗畅 , 刘承君 , 张峰 , 章华 . 吸气式高超声速飞行器预设反演鲁棒控制[J]. 弹箭与制导学报, 2021 , 41(2) : 114 -119 . DOI: 10.15892/j.cnki.djzdxb.2021.02.024

Abstract

A prescribed performance back-stepping robust control approach is presented for the dynamical model of generic air-breathing hypersonic vehicle. A performance function characterizing the error convergence rate and maximum overshoot is designed for the tracking error transformation under the back-stepping framework. To enhance the robustness of back-stepping controller, the novel disturbance observers based on the modified arctangent-based tracking differentiators are devised to estimate the uncertainties of model. The simulation results show that the transient performance of the control system can reach the prescribed performance.

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