DocumentCode
2269787
Title
Application of the combined method of adaptive control to an aircraft control system
Author
Rao, M.P.R.V. ; Wong, M.T.F.
Author_Institution
Ulster Univ., Jordanstown, UK
fYear
1991
fDate
25-28 Mar 1991
Firstpage
539
Abstract
Advances in adaptive control theory have been reviving its application to the aircraft control problem. A combination of direct and indirect methods of adaptive control is applied to the pitch rate control system problem in the paper. The scheme used employs integral form adaptive laws. The paper presents the mathematics of the scheme; simulation results (using SIMNON package) for different flight conditions. The scheme offers the advantages of the combined method of adaptive control
Keywords
adaptive control; aerospace simulation; aircraft control; adaptive control; aircraft control system; combined method; direct methods; flight conditions; indirect methods; pitch rate control system;
fLanguage
English
Publisher
iet
Conference_Titel
Control 1991. Control '91., International Conference on
Conference_Location
Edinburgh
Print_ISBN
0-85296-509-5
Type
conf
Filename
98506
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