DocumentCode :
3469170
Title :
Stability analysis for a class of linear controllers under control constraints
Author :
Dolphus, R.M. ; Schmitendorf, W.E.
Author_Institution :
Dept. of Mech. & Aerosp. Eng., California Univ., Irvine, CA, USA
fYear :
1991
fDate :
11-13 Dec 1991
Firstpage :
77
Abstract :
The authors present a method for analyzing a system for stability when control magnitude constraints are introduced. They start with a given linear full state feedback controller of a certain form which stabilizes the unconstrained system. For the constrained system, where the control is obtained by saturating the linear control, stability is shown as a tradeoff between the size of the initial condition set and the size of the control constraints. As an example the linearized equations of motion for a satellite in a circular equatorial orbit are considered
Keywords :
control system analysis; feedback; linear systems; stability; circular equatorial orbit; control system analysis; linear full state feedback controller; linearized equations of motion; satellite; stability analysis; unconstrained system; Aerospace engineering; Control systems; Equations; Linear feedback control systems; Lyapunov method; Optimal control; Riccati equations; Satellites; Size control; Stability analysis; State feedback; Strain control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 1991., Proceedings of the 30th IEEE Conference on
Conference_Location :
Brighton
Print_ISBN :
0-7803-0450-0
Type :
conf
DOI :
10.1109/CDC.1991.261258
Filename :
261258
Link To Document :
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