航空学报 > 1991, Vol. 12 Issue (4): 166-170

飞机大迎角稳定性和状态矢量传播灵敏度研究

李季陆, 何植岱   

  1. 西北工业大学
  • 收稿日期:1988-05-01 修回日期:1990-11-01 出版日期:1991-04-25 发布日期:1991-04-25

A STUDY ON THE STABILITY OF AIRCRAFT AT HIGH ANGLES-OF-ATTACK AND STATE VECTOR PROPAGATION SENSITIVITY

Li Jilu, He Zhidai   

  1. Northwestern Pol ytechnical University
  • Received:1988-05-01 Revised:1990-11-01 Online:1991-04-25 Published:1991-04-25

关键词: 大迎角, 稳定性, 传播灵敏度

Abstract: Based on the study of a typical modern fighterat high angles-of-attack according to Bifurcation Analysis and Catastrophe Theory Methodology (BACTM), the fourth Runge-Kutta scheme is adopted to examine the state vector propagation sensitivity during the aircraft's motion. The causes of some jump phenomena of motion are analysed.

Key words: high anales-of-attack, stability, propagation sensitivity