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
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