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弹箭与制导学报 >

2020 , Vol. 40 >Issue 1: 165 - 169

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2020.01.034

受控制量及状态约束的高超声速飞行器 姿态控制方法研究

  • 仲秦 1 ,
  • 闫杰 1 ,
  • 张晓峰 1 ,
  • 武文斌 2
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  • 1 西北工业大学航天学院, 西安 710072
  • 2 西安现代控制技术研究所,西安 710065

仲秦(1987-),女,陕西西安人,博士研究生,研究方向:飞行器制导控制系统设计及仿真、导弹武器系统性能评估、高超声速飞行器建模及控制技术研究。

收稿日期: 2019-01-19

  网络出版日期: 2025-05-30

基金资助

国家自然科学基金(61503302)

收起

The Research on Flight Control of Hypersonic Vehicle Constrained by States and Control Input

  • ZHONG Qin 1 ,
  • YAN Jie 1 ,
  • ZHANG Xiaofeng 1 ,
  • WU Wenbin 2
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  • 1 School of Astronautics, Northwestern Polytechnic University, Xi’an 710072, China
  • 2 Xi’an Modern Control Technology Research Institute, Xi’an 710065, China

Received date: 2019-01-19

  Online published: 2025-05-30

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摘要

为满足高超声速飞行器对超燃冲压发动机的限制,其飞行控制是受控制量和状态约束的跟踪控制。文中采用单向辅助面控制设计方法,将系统误差设置成正不变集的边界,令系统状态从任意初始位置单调收敛到指令状态,从而使跟踪过程系统状态满足约束。通过设置误差积分初值,引入控制量约束,解不等式得到控制约束的系统初始状态范围。完成了受控制量及状态约束的跟踪控制,并通过飞行器纵向姿态控制器的设计验证了该方法的有效性。

关键词： 状态约束控制; 单向辅助面控制; 高超声速飞行器

本文引用格式

仲秦 , 闫杰 , 张晓峰 , 武文斌 . 受控制量及状态约束的高超声速飞行器 姿态控制方法研究[J]. 弹箭与制导学报, 2020 , 40(1) : 165 -169 . DOI: 10.15892/j.cnki.djzdxb.2020.01.034

Abstract

In order to meet the restriction of hypersonic vehicle on scramjet, its flight control is a tracking control with control variables and state constraints. In this paper, the design method of one-way auxiliary surface control is used to set the system error to the boundary of positive invariant set, so that the system state can converge monotonously from any initial position to the instruction state, so that the system state of tracking process meets the constraints. By setting the initial value of error integral and introducing control constraints, the initial state range of the system with control constraints is obtained by solving inequalities. Through the above method, the tracking control constrained by control variables and states is completed, and the effectiveness of the method is verified by the design of the longitudinal attitude controller of the aircraft.

Key words： state constrained control; unidirectional auxiliary surface control; hypersonic vehicle

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参考文献

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