DocumentCode
2106516
Title
Continuous output tracking control of a class of nonlinear systems
Author
Song, Y.D. ; Homaifar, A. ; Lai, H.Y.
Author_Institution
NASA CORE for Aerosp. Res., North Carolina A&T State Univ., Greensboro, NC, USA
fYear
1993
fDate
15-17 Dec 1993
Firstpage
2131
Abstract
Inverse dynamic tracking control problem of a class of nonlinear systems arising from aerospace and mechanical engineering is addressed. Because modelling uncertainties and external disturbances are always present in these systems, inverse dynamics technique is not applicable directly. A compensated inverse dynamics approach is proposed to account for the effect of uncertainties. The compensation is achieved by adaptive and robust schemes. Application of the proposed strategy to the vibration suppression of a two-bay flexible truss structure is presented
Keywords
adaptive control; aerospace control; compensation; nonlinear systems; stability; tracking; vibration control; adaptive control; aerospace engineering; compensation; continuous output tracking control; external disturbances; inverse dynamic tracking; mechanical engineering; modelling uncertainties; nonlinear systems; robust control; two-bay flexible truss structure; vibration suppression; Aerodynamics; Aerospace control; Aerospace engineering; Control systems; Mechanical engineering; Nonlinear control systems; Nonlinear systems; Robustness; Uncertainty; Vibrations;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1993., Proceedings of the 32nd IEEE Conference on
Conference_Location
San Antonio, TX
Print_ISBN
0-7803-1298-8
Type
conf
DOI
10.1109/CDC.1993.325572
Filename
325572
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