DocumentCode :
489634
Title :
Turbulence/Gust Alleviation using Spoiler Control
Author :
Sun, X.D. ; Allwright, J.C.
Author_Institution :
Department of Aeronautics, Imperial College, London SW7 2BY, U.K.
fYear :
1992
fDate :
24-26 June 1992
Firstpage :
1544
Lastpage :
1545
Abstract :
This paper presents recent work on applications of spoiler control to aircraft manoeuvring enhancement and gust alleviation. The nonlinear inverse dynamics control technique is applied to the synthesis of a decoupled model-following flight control system for an aircraft with spoilers. The effectiveness of spoiler control on turbulence/gust alleviation is examined by some simulations of landing approach in turbulence.
Keywords :
Aerodynamics; Aerospace control; Aircraft; Control system synthesis; Educational institutions; Elevators; Erbium; Nonlinear control systems; Nonlinear dynamical systems; Regulators; Aerospace control; flight control systems; inverse dynamics; mathematics and mathematical modelling; nonlinear control systems; simulation technology;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1992
Conference_Location :
Chicago, IL, USA
Print_ISBN :
0-7803-0210-9
Type :
conf
Filename :
4792367
Link To Document :
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