DocumentCode :
2761266
Title :
The design of LQG and H controllers for use in active vibration control and narrow band disturbance rejection
Author :
Connolly, Allan J. ; Green, Michael ; Chicharo, Joe F. ; Bitmead, Robert R.
Author_Institution :
Dept. of Syst. Eng., Australian Nat. Univ., Canberra, ACT, Australia
Volume :
3
fYear :
1995
fDate :
13-15 Dec 1995
Firstpage :
2982
Abstract :
This paper develops an H design method for narrow band disturbance rejection. The method is based on the LQG approach via disturbance modelling given in De Nicolao (1992). These LQG and H approaches to the narrow band disturbance rejection problem are then applied to a helicopter active vibration control problem
Keywords :
H control; aircraft control; control system synthesis; helicopters; linear quadratic Gaussian control; vibration control; H controllers; LQG control; active vibration control; disturbance modelling; helicopter; narrow band disturbance rejection; Australia; Damping; Delta modulation; Frequency; H infinity control; Helicopters; Narrowband; Servomechanisms; Strips; Vibration control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 1995., Proceedings of the 34th IEEE Conference on
Conference_Location :
New Orleans, LA
ISSN :
0191-2216
Print_ISBN :
0-7803-2685-7
Type :
conf
DOI :
10.1109/CDC.1995.478598
Filename :
478598
Link To Document :
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