DocumentCode :
3250291
Title :
LQG/LTR controller design using a reduced order model
Author :
Prakash, Rajiva ; Rao, S. Vittal
Author_Institution :
Dept. of Electr. Eng., Missouri Univ., Rolla, MO, USA
fYear :
1989
fDate :
0-0 1989
Firstpage :
343
Lastpage :
346
Abstract :
A specific robust controller design procedure, linear quadratic Gaussian with loop transfer recovery (LQG/LTR), is studied. LQG/LTR design using a reduced-order model is performed. The error due to the use of the reduced model is accounted for by computing multiplicative error. All closed right half plane modes of the given system are included in the reduced-order model. The reduced-order LQG/LTR controller design procedure is applied to the problem of lateral attitude control of a drone aircraft. The case study demonstrates the reduction/design steps for a practical problem.<>
Keywords :
control system synthesis; controllers; LQG/LTR controller design; drone aircraft; lateral attitude control; linear quadratic Gaussian; loop transfer recovery; multiplicative error; reduced order model; robust controller design procedure;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Systems Engineering, 1989., IEEE International Conference on
Conference_Location :
Fairborn, OH, USA
Type :
conf
DOI :
10.1109/ICSYSE.1989.48686
Filename :
48686
Link To Document :
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