DocumentCode
2429231
Title
Successive approximation for H∞
Author
Liu, Yong ; Yedavalli, Rama K.
Author_Institution
Dept. of Aeronaut. & Astronaut. Eng., Ohio State Univ., Columbus, OH, USA
Volume
3
fYear
1994
fDate
29 June-1 July 1994
Firstpage
2757
Abstract
This paper gives three new algorithms for the H∞ control problem based on the idea of successive approximation. Unlike the generally used solution procedure based on the central Riccati equation, the proposed algorithms use a gain-updating scheme which has the advantage of connecting any stabilizing gain to the H∞ optimal gain. Various properties of the updating scheme are proved. In particular, it is shown under mild conditions that the existence, stabilizability and monotonicity of the solutions of the Riccati equation at each step are naturally guaranteed. The algorithms only involve an H∞ norm evaluation problem at each step and are proved to be convergent to the central solution for the given parameter of H∞ norm bound. These algorithms are particularly effective when the system order is large. A numerical example is given to illustrate the proposed algorithms.
Keywords
H∞ control; Riccati equations; approximation theory; control system analysis; stability; state-space methods; H∞ control; H∞ norm bound; Riccati equation; gain-updating scheme; monotonicity; optimal control; stability; stabilizability; stabilizing gain; state space; successive approximation; Aerospace engineering; Approximation algorithms; Centralized control; Control systems; Joining processes; Optimal control; Prediction algorithms; Riccati equations; Search methods; State feedback;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1994
Print_ISBN
0-7803-1783-1
Type
conf
DOI
10.1109/ACC.1994.735070
Filename
735070
Link To Document