航空学报 > 1993, Vol. 14 Issue (9): 550-555

飞机横侧向系统的INA设计和鲁棒性分析

马晓军, 程鹏   

  1. 北京航空航天大学301教研室,北京,100083
  • 收稿日期:1990-10-04 修回日期:1992-07-04 出版日期:1993-09-25 发布日期:1993-09-25

AN INA DESIGN AND ROBUST ANALYSIS OF THE LATERAL FLIGHT CONTROL SYSTEM

Ma Xiao-jun, Cheng Peng   

  1. Faculty 301 oj Beijing University of Aeronautics and Astronautics, Beijing, 100083
  • Received:1990-10-04 Revised:1992-07-04 Online:1993-09-25 Published:1993-09-25

摘要: 用INA方法设计某飞机的横侧向控制系统,数学仿真的结果说明针对高度H=10 000m,Ma为0.9的飞行状态设计的横侧向控制器同样适用于高度H=10 000m,Ma为1.5的飞行状态。最后用鲁棒INA方法对设计进行了鲁棒性分析,说明该设计提高了模型误差可允许的界限。

关键词: 对角优势, 鲁棒性, 鲁棒对角优势

Abstract: In this paper, the lateral flight control system is designed in INA methodology. The result of simulation shows that the lateral controler designed for H= 10 000 metres, Ma = 0.9 can be used in the situation of H= 10 000 metres, Ma=1.5. Finally, robust analysis is done in robust INA methodology, which shows that the design enhances the admissible bound of the model error. All data are calculated by IBM PC computer. Gershgorin bands, Ostrowski bands and robust Gershgorin bands, robust Ostrowski bands are drawn by MP 1000 drawing instrument.

Key words: diagonal dominance, robust, roust diagonal dominance