DocumentCode :
754515
Title :
VSTOL first flight on an H/sub infinity / control law
Author :
Hyde, R.A. ; Glover, K. ; Shanks, G.T.
Author_Institution :
Dept. of Eng., Cambridge Univ., UK
Volume :
6
Issue :
1
fYear :
1995
Firstpage :
11
Lastpage :
16
Abstract :
An H/sub infinity / control law has been successfully flight tested on the DRA Bedford Harrier. This and subsequent flight tests demonstrated the practicality and power of H/sub infinity / as a design tool for systems with multiple inputs and outputs. The technique has potential both to reduce design time, and to improve robustness and performance for such systems. This article discusses the development of the control law and some of the challenging implementation issues which had to be addressed in order to bridge the gap between theory and practice.<>
Keywords :
aerospace control; aircraft control; control system CAD; military aircraft; DRA Bedford Harrier; H/sub infinity / control law; VSTOL; advanced short take off and vertical landing aircraft; aerodynamic control; control law; design time; design tool; flight control; flight tested; multiple inputs; multiple outputs; performance; robustness; Aerospace control; Aircraft control; Control systems; Design automation; Military aircraft;
fLanguage :
English
Journal_Title :
Computing & Control Engineering Journal
Publisher :
iet
ISSN :
0956-3385
Type :
jour
DOI :
10.1049/cce:19950107
Filename :
372707
Link To Document :
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