DocumentCode :
2703309
Title :
Output tracking with nonhyperbolic and near nonhyperbolic internal dynamics: helicopter hover control
Author :
Devasia, Santosh
Author_Institution :
Dept. of Mech. Eng., Utah Univ., Salt Lake City, UT, USA
Volume :
3
fYear :
1997
fDate :
4-6 Jun 1997
Firstpage :
1439
Abstract :
A technique to achieve output tracking for nonminimum phase linear systems with nonhyperbolic and near nonhyperbolic internal dynamics is presented. This approach integrates stable inversion techniques, that achieve exact-tracking, with approximation techniques, that modify the internal dynamics to achieve desirable performance. Such modification of the internal dynamics is used (a) to remove nonhyperbolicity which is an obstruction to applying stable inversion techniques and (b) to reduce large preactuation times needed to apply stable inversion for near nonhyperbolic cases. The method is applied to an example helicopter hover control problem with near nonhyperbolic internal dynamics for illustrating the tradeoff between exact tracking and reduction of preactuation time
Keywords :
approximation theory; dynamics; feedforward; helicopters; linear systems; poles and zeros; stability; state feedback; tracking; velocity control; approximation techniques; helicopter hover control; nonhyperbolic internal dynamics; nonminimum phase linear systems; output tracking; preactuation times; stable inversion techniques; Aerospace control; Air traffic control; Aircraft manufacture; Control systems; Flexible structures; Helicopters; Linear systems; Mechanical engineering; Regulators; Robot control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1997. Proceedings of the 1997
Conference_Location :
Albuquerque, NM
ISSN :
0743-1619
Print_ISBN :
0-7803-3832-4
Type :
conf
DOI :
10.1109/ACC.1997.610689
Filename :
610689
Link To Document :
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