DYNAMIC INVERSION - AN EVOLVING METHODOLOGY FOR FLIGHT CONTROL DESIGN

被引：200
|
作者：
ENNS, D
BUGAJSKI, D
HENDRICK, R
STEIN, G
机构：
[1] UNIV MINNESOTA,DEPT AEROSP ENGN & MECH,MINNEAPOLIS,MN 55455
[2] MIT,CAMBRIDGE,MA 02139
来源：
INTERNATIONAL JOURNAL OF CONTROL | 1994年 / 59卷 / 01期
关键词：
D O I：
10.1080/00207179408923070
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
This paper describes nonlinear dynamic inversion as an alternative design method for flight controls. The method is illustrated with super-manoeuvring control laws for the F-18 high angle-of-attack research vehicle.
引用
收藏
页码：71 / 91
页数：21
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