DocumentCode
280620
Title
An engineering approach to control design and analysis for flexible aircraft
Author
Kaynes, I.U.
Author_Institution
Dept. of Mater. & Structures, Minist. of Defence, R. Aerosp. Establ., Farnborough, UK
fYear
1990
fDate
32910
Firstpage
42491
Lastpage
42492
Abstract
The objectives of this research at the Royal Aerospace Establishment, Farnborough, were the improvement of aeroelastic modelling techniques, the development of design methods for active control technology (ACT), and the assessment of the impact of ACT on aircraft structures. Related experimental have included the measurements of aircraft responses in flight on VC10 and tornado aircraft, and experiments to demonstrate the implementation of control system on wind tunnel models
Keywords
aircraft control; control system synthesis; Royal Aerospace Establishment; VC10; active control technology; aeroelastic modelling; aircraft control; control design; flexible aircraft; tornado;
fLanguage
English
Publisher
iet
Conference_Titel
Integrating Control System Design with the Analysis of Flexible Structures, IEE Colloquium on
Conference_Location
London
Type
conf
Filename
190974
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