系统工程与电子技术

• 制导、导航与控制 • 上一篇    下一篇

基于干扰估计的高超声速飞行器鲁棒控制方法

张银辉, 杨华波, 江振宇, 张为华   

  1. (国防科学技术大学航天科学与工程学院, 湖南 长沙 410073)
  • 出版日期:2016-03-25 发布日期:2010-01-03

Robust control of hypersonic flight vehicle based on disturbance estimation

ZHANG Yin-hui, YANG Hua-bo, JIANG Zhen-yu, ZHANG Wei-hua   

  1. (College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China)
  • Online:2016-03-25 Published:2010-01-03

摘要:

针对高超声速飞行器高度与速度跟踪所面临的参数不确定与外界干扰问题,提出基于干扰估计的鲁棒控制律设计方法。首先建立含参数不确定与外界干扰的高超声速飞行器模型;而后基于动态逆思想,将动力学模型进行线性化,并将由参数不确定与外界干扰对系统造成的总效果看作系统总干扰,从而引入线性扩张状态观测器实现对系统状态及总干扰的估计;最后考虑总干扰作用,提出具有鲁棒性能的动态逆控制律与滑模控制律。通过与传统控制律进行对比仿真,结果表明所设计的两种鲁棒控制器只需在原有方法基础上进行简单改进,即可较大程度提高对系统参数不确定与外界干扰的鲁棒性,具有良好的跟踪性能。

Abstract:

A robust control method based on disturbance estimation is proposed in order to address the altitude and velocity tracking problem for hypersonic flight vehicles with parameter uncertainty and external disturbance. Firstly, a flight vehicle mode is established considering parameter uncertainties and external disturbances. And then, the model is linearized based on the dynamic inversion control method. The total effect of the uncertainties and disturbances for the system is regarded as the lumped disturbance, which is then estimated together with the system states by the linear extended state observer. Subsequently, the lumped disturbance is integrated into the baseline controller, and disturbance estimation based robust dynamic inversion control and sliding mode control are proposed. Compared with baseline controllers, the proposed two robust controllers not only enhance the robustness against parameter uncertainties and external disturbances, bust also improve the tracking performance.