DocumentCode
335305
Title
A nonlinear application of a Lyapunov technique for assuring global performance bounds
Author
Helmersson, Anders
Author_Institution
Dept. of Electr. Eng., Linkoping Univ., Sweden
Volume
1
fYear
1994
fDate
29 June-1 July 1994
Firstpage
954
Abstract
In this paper we consider the stability and performance problem of nonlinear systems using a Lyapunov technique. The upper or lower bounds can be provided assuming that a Lyapunov function satisfies a Hamiltonian inequality for all admissible states. Also, suboptimal control laws with guaranteed performance bounds can be derived with this technique. The technique has been applied on rate and attitude control for sounding rockets. As an example, a rate control algorithm is elaborated showing the main ideas presented in this paper: (1) the Lyapunov function provides a global performance bound; (2) a control law is derived based on the Lyapunov function; and (3) the candidate Lyapunov function is parametrized and improved bounds are obtained using parameter optimization.
Keywords
Lyapunov methods; attitude control; nonlinear systems; optimal control; rockets; stability; Lyapunov function; attitude control; global performance bound; lower bounds; nonlinear systems; optimal control; rate control; sounding rockets; stability; upper bounds; Control systems; Equations; Lyapunov method; Nonlinear control systems; Nonlinear systems; Optimal control; Rockets; Space vehicles; Stability; Upper bound;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1994
Print_ISBN
0-7803-1783-1
Type
conf
DOI
10.1109/ACC.1994.751885
Filename
751885
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