DocumentCode :
306713
Title :
Bounded tracking for nonminimum phase nonlinear systems with fast zero dynamics
Author :
Tomlin, C.J. ; Sastry, S.S.
Author_Institution :
Dept. of Electr. Eng. & Comput. Sci., California Univ., Berkeley, CA, USA
Volume :
2
fYear :
1996
fDate :
11-13 Dec 1996
Firstpage :
2058
Abstract :
We derive tracking control laws for nonminimum phase nonlinear systems with both fast and slow, possibly unstable, zero dynamics. The fast zero dynamics arise from a perturbation of a nominal system. These fast zeros can be problematic in that they may be in the right half plane and may cause large magnitude tracking control inputs. In this paper, we combine the ideas from work of Hunt, Meyer, and Su (1995)with that of Devasia, Paden, and Chen (1996) on an asymptotic tracking procedure for nonminimum phase nonlinear systems. We give (somewhat subtle) conditions under which the tracking control input is bounded as the magnitude of the perturbation of the nominal system becomes zero. Explicit bounds on the control inputs are calculated using some interesting non-standard singular perturbation techniques. The method is applied to the simplified planar dynamics of VTOL and CTOL aircraft
Keywords :
aircraft control; nonlinear control systems; perturbation techniques; singularly perturbed systems; tracking; CTOL aircraft; VTOL aircraft; asymptotic tracking; bounded tracking; explicit bounds; fast zero dynamics; large magnitude tracking control inputs; nominal system; nonminimum phase nonlinear systems; nonstandard singular perturbation techniques; simplified planar dynamics; tracking control laws; Aerospace control; Aircraft; Control systems; Ear; MIMO; Nonlinear control systems; Nonlinear dynamical systems; Nonlinear systems; Perturbation methods; Regulators;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 1996., Proceedings of the 35th IEEE Conference on
Conference_Location :
Kobe
ISSN :
0191-2216
Print_ISBN :
0-7803-3590-2
Type :
conf
DOI :
10.1109/CDC.1996.572889
Filename :
572889
Link To Document :
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