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