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 :
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