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.
Recommended Citation
R. Prakash and V. s. Rao, "LQG/LTR Controller Design Using A Reduced Order Model,", pp. 343 - 346 Institute of Electrical and Electronics Engineers, Jan 1989.
The definitive version is available at https://doi.org/10.1109/icsyse.1989.48686
Department(s)
Electrical and Computer Engineering
Document Type
Article - Conference proceedings
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 2023 Institute of Electrical and Electronics Engineers, All rights reserved.
Publication Date
01 Jan 1989
