DocumentCode :
2428811
Title :
Optimal tradeoff between H2 performance and tracking accuracy in servocompensator synthesis
Author :
Sparks, Andrew G. ; Bernstein, Dennis S.
Author_Institution :
Dept. of Aerosp. Eng., Michigan Univ., Ann Arbor, MI, USA
Volume :
3
fYear :
1994
fDate :
29 June-1 July 1994
Firstpage :
2675
Abstract :
The problem of optimal H2 disturbance rejection while tracking uncertain constant or sinusoidal reference commands is considered. The internal model principle is used to ensure that the tracking error approaches zero asymptotically. Necessary conditions are given for controllers that minimize an H2 disturbance rejection cost plus a worst-case integral square tracking error for transient tracking performance. The necessary conditions provide expressions for the gradients of the cost with respect to each of the control gains. These expressions are then used in a quasi-Newton gradient search algorithm to determine the optimal feedback gains. Numerical examples demonstrate the tradeoff between the two competing objectives in the cost function.
Keywords :
Newton method; compensation; conjugate gradient methods; control system synthesis; feedback; model reference adaptive control systems; optimal control; search problems; servomechanisms; tracking; H2 disturbance rejection cost minimization; H2 performance; constant reference commands; internal model principle; optimal H2 disturbance rejection; optimal feedback gains; optimal tradeoff; quasi-Newton gradient search algorithm; servocompensator synthesis; sinusoidal reference commands; tracking accuracy; tracking error; uncertain commands; worst-case integral square tracking error; Aerodynamics; Cost function; Error correction; Feedback; Frequency; Hydrogen; Polynomials; Servomechanisms; Sparks; Steady-state;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1994
Print_ISBN :
0-7803-1783-1
Type :
conf
DOI :
10.1109/ACC.1994.735047
Filename :
735047
Link To Document :
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