航空学报 > 1986, Vol. 7 Issue (6): 566-574

颤振主动抑制控制律的研究

王卫平, 顾仲权, 朱德懋   

  1. 南京航空学院
  • 收稿日期:1986-01-18 修回日期:1900-01-01 出版日期:1986-12-25 发布日期:1986-12-25

RESEARCH ON CONTROL LAW FOR ACTIVE FLUTTER SUPPRESSION

Wang Weiping, Gu Zhongquan, Zhu Demao   

  1. Nanjing Aeronautical Institute
  • Received:1986-01-18 Revised:1900-01-01 Online:1986-12-25 Published:1986-12-25

摘要: 本文以一个小展弦比三角机翼的风洞模型为研究对象,研究颤振主动抑制技术,包括建立伺服气动弹性系统的数学模型,次最优输出反馈控制律的综合和分析。

Abstract: This paper studies the technology of active flutter suppression by using the wind-tunnel model of a delfa wing with low-aspect ratio as research specimen. The researches include the establishment of mathematical model for a servo-aeroelastic system and the synthesis and analysis of sub-optimal output feedback control laws for active flutter suppression.