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
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