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
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