DocumentCode :
2427610
Title :
Design of H2 and H controllers with two degrees of freedom
Author :
Christen, Urs ; Weilenmann, Martin E. ; Geering, Hans P.
Author_Institution :
Meas. & Control Lab., Swiss Federal Inst. of Technol., Zurich, Switzerland
Volume :
3
fYear :
1994
fDate :
29 June-1 July 1994
Firstpage :
2391
Abstract :
The tracking behavior of many feedback control systems can be improved by using a compensator with two degrees of freedom which processes the reference signal independently of the plant output signal, e.g., the reference signal can be processed by a static prefilter. This is described in the first part of this paper dealing with LQG/LTR and H2 controllers. With H methods, it is easy to design more sophisticated, dynamic feedforward controllers. They can be developed either in a second step, when the loop is already closed by a feedback compensator, or in one step together with the H feedback part of the compensator. This latter possibility has the advantage that only one observer is needed for the two parts of the controller, thus the number of states of the complete compensator is minimized. An application of these design configurations to a helicopter is shown. Step responses without overshoot are achieved for position control.
Keywords :
H control; aircraft control; compensation; control system synthesis; feedback; feedforward; helicopters; linear quadratic Gaussian control; step response; tracking; H controllers; H feedback; H2 controllers; LQG/LTR; compensator; design configurations; dynamic feedforward controllers; feedback compensator; feedback control systems; helicopter; observer; position control; static prefilter; step responses; tracking behavior; two degrees of freedom; Control systems; Design methodology; Filters; Hydrogen; Motion control; Noise shaping; Regulators; Rotors; Tail; Transfer functions;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1994
Print_ISBN :
0-7803-1783-1
Type :
conf
DOI :
10.1109/ACC.1994.734987
Filename :
734987
Link To Document :
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