航空学报 > 1997, Vol. 18 Issue (5): 591-594

模型参考时变滑态变结构控制方法研究

黄万伟, 周凤岐   

  1. 西北工业大学803教研室, 西安, 710072
  • 收稿日期:1997-01-15 修回日期:1997-04-13 出版日期:1997-10-25 发布日期:1997-10-25

INVESTIGATION OF MODEL REFERENCE VARIABLE STRUCTURE CONTROL WITH TIME VARYING SLIDING MODE

Huang Wanwei, Zhou Fengqi   

  1. Faculty 803, Northwestern Polytechnical University,Xi'an,710072
  • Received:1997-01-15 Revised:1997-04-13 Online:1997-10-25 Published:1997-10-25

摘要:

针对一类特殊线性时变系统,提出了一种新的模型参考时变滑态结构控制器设计方法。能较好地适应时变系统参数大范围的变化,提高控制精度和控制效益。利用该方法设计了某型BTT导弹俯仰-偏航通道自动驾驶仪变结构控制律,取得了很好的控制效果。

关键词: 线性时变系统, 时变滑态, 模型参考变结构控制器

Abstract:

A new method of model reference variable structure control with sliding mode (MRVSCSM) is proposed for a class of time varying linear system. This method employs the time varying reference model and time varying switch function to adapt the largely change of system parameters, and to improve efficiency and accuracy of control. This method is applied to design control laws of Pitch/Yaw channels autopilot for BTT missiles. The digital simulation shows that the system has good performance and robustness.

Key words: time-varying linear system, time-varying sliding mode, model reference variable structure controller

中图分类号: