DocumentCode :
706803
Title :
An LPV-LMI approach to generalised active control of vibrations in helicopters
Author :
Bittanti, S. ; Cuzzola, F.A. ; Lovera, M. ; Lussana, N.
Author_Institution :
Dipt. di Elettron. e Inf., Politec. di Milano, Milan, Italy
fYear :
1999
fDate :
Aug. 31 1999-Sept. 3 1999
Firstpage :
2783
Lastpage :
2788
Abstract :
In this paper the problem of active control of vibrations in helicopters is faced in a very general way. Precisely, we consider the case when the aircraft moves according to a possibly varying forward velocity. The problem is then more complex that the one encountered in hover or in forward flight. We tackle the general problem by means of an LPV (Linear Parametrically-Varying) approach, complemented with concepts drawn from LMI (Linear Matrix Inequalities) realm, H2-filtering and H control. The simulations indicate that the overall controller so obtained is most promising.
Keywords :
H control; aircraft control; helicopters; linear matrix inequalities; linear parameter varying systems; vibration control; H control; H2-filtering; LPV-LMI approach; aircraft; complex problem; forward flight; general problem; generalised active vibration control problem; helicopters; hover; linear matrix inequalities; linear parametrically-varying approach; possibly-varying forward velocity; Atmospheric modeling; Blades; Helicopters; Mathematical model; Rotors; Vibrations; Active control of vibrations; LMI (Linear Matrix Inequalities); Linear Parametrically-Varying systems;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (ECC), 1999 European
Conference_Location :
Karlsruhe
Print_ISBN :
978-3-9524173-5-5
Type :
conf
Filename :
7099748
Link To Document :
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