航空学报 > 1996, Vol. 17 Issue (2): 129-136

H~∞方法在鲁棒飞控系统设计中的应用

王炎生, 陈宗基   

  1. 北京航空航天大学自控系,北京,100083
  • 收稿日期:1994-03-05 修回日期:1995-01-13 出版日期:1996-04-25 发布日期:1996-04-25

SURVEY ON THE APPLICATIONS OF H~∞ METHOD IN ROBUST FLIGHT CONTROL SYSTEMS DESIGN

Wang Yansheng, Chen Zongji   

  1. Dept. of Automatic Control, Beijing University of Aeronautics and Astronautics, Beijing,100083
  • Received:1994-03-05 Revised:1995-01-13 Online:1996-04-25 Published:1996-04-25

摘要: 首先介绍具有良好鲁棒稳定性和鲁棒性能的 H∞方法 ,然后综述几年来 H∞方法在鲁棒飞控系统设计中的应用研究 ,详细说明 H∞ 鲁棒飞控系统设计问题的形成和求解过程 ,并分析模型 /控制器降阶 ,结构不确定性和非结构不确定性的同时镇定 ,多模型设计等与 H∞方法相配合的设计技术的使用

关键词: 系统稳定性, 最优控制, 鲁棒性, 飞行控制

Abstract: First,this paper briefly introduces the H ∞ methods which have satisfactory robust stability and robust performance, and then it surveys the application studies of H ∞ methods in robust flight control systems design in recent years,which includes showing how to formulate and solve the H ∞ robust flight control system design problem, and analysing the design techniques, such as model/controller reduction, simultaneous stabilization of the structured and unstructured uncertaintes and multi models design techniques which are suitable for H ∞ methods.

Key words: system stabilit, optimum contro, robustnes, flight control

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