| 注册
首页|期刊导航|控制理论与应用|抑制机翼主动颤振的输出微分调节器

抑制机翼主动颤振的输出微分调节器

张子健 徐敏 陈士橹 罗翔

控制理论与应用2009,Vol.26Issue(10):1143-1147,5.
控制理论与应用2009,Vol.26Issue(10):1143-1147,5.

抑制机翼主动颤振的输出微分调节器

Output-rate-weighted regulator for suppressing active flutter on flapping wing

张子健 1徐敏 1陈士橹 1罗翔2

作者信息

  • 1. 西北工业大学,航天学院,陕西,西安,710072
  • 2. 西北工业大学,365研究所,陕西,西安,710072
  • 折叠

摘要

Abstract

The suppression of active flutter on a flapping wing is a major topic in the design of modern flexible airplanes; but the traditional linear quadratic optimal regulator(LQRY) based on the minimization of the weighted output doesn't work well for this purpose. A new optimal regulator based on the minimization of the output rate weighted minimizing(ORW) is developed. Being different from the LQRY, this regulator makes use of more system information. It minimizes the time-rate of the output, which is not available for a direct measurement, thereby suppressing the flutter more quickly. Simulation is performed on a Benchmark Active Control Technology(BACT) system by using the ORW regulator and the LQRY regulator respectively. The results show that the ORW regulator provides a better performance.

关键词

颤振抑制/最优控制/输出微分

Key words

flutter suppression/ optimal control/ output rate weighted

分类

航空航天

引用本文复制引用

张子健,徐敏,陈士橹,罗翔..抑制机翼主动颤振的输出微分调节器[J].控制理论与应用,2009,26(10):1143-1147,5.

基金项目

高等学校博士学科点专向科研基金资助项目(20070699054) (20070699054)

国家自然科学基金重大研究计划资助项目(90405002). (90405002)

控制理论与应用

OA北大核心CSCDCSTPCD

1000-8152

访问量0
|
下载量0
段落导航相关论文