DocumentCode :
489513
Title :
A Feedback Descent Method for Solving Constrained LQG Control Problems
Author :
Beseler, Jan ; Chow, Joe H. ; Minto, K.D.
Author_Institution :
GE Aircraft Engine, Lynn, MA. 01910
fYear :
1992
fDate :
24-26 June 1992
Firstpage :
1044
Lastpage :
1048
Abstract :
This paper presents a new method for the numerical solution of LQG optimal control problems subject to constraints. In general, solutions to these problems necessarily satisfy a set of coupled Lyapunov and/or Riccati equations. These equations are solved in an iterative manner based on a quasi-Newton type algorithm. Key features of the method are the simplicity afforded in developing iterative algorithms satisfying the necessary conditions for solution of such problems, and the speed and efficiency of these algorithms. The technique is illustrated for the optimal static output feedback problem and the optimal LQG problem with an H¿ norm bound on a closed-loop transfer function.
Keywords :
Aircraft propulsion; Helium; Newton method; Optimal control; Output feedback; Research and development; Riccati equations; Robustness; Transfer functions; White noise;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1992
Conference_Location :
Chicago, IL, USA
Print_ISBN :
0-7803-0210-9
Type :
conf
Filename :
4792244
Link To Document :
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