DYNAMIC INVERSION - AN EVOLVING METHODOLOGY FOR FLIGHT CONTROL DESIGN

被引：224

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

页码：71 / 91

页数：21

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