DocumentCode
2509313
Title
A preliminary longitudinal aircraft control design by applying the multivariable frequency matching technique
Author
Pujara, L.R. ; Shabbarhussein, Mnkhtar
Author_Institution
Dept. of Electr. Eng., Wright State Univ., Dayton, OH, USA
fYear
1994
fDate
24-26 Aug 1994
Firstpage
83
Abstract
In this paper, a preliminary longitudinal control system for the YF-16 CCV aircraft is designed to satisfy its flying qualities. This objective is achieved by applying the multivariable frequency matching technique of control systems designed and developed by the authors. This technique is in the spirit of `model following´ strategy carried out in the frequency domain
Keywords
aircraft control; attitude control; closed loop systems; control system synthesis; feedback; multivariable control systems; transfer function matrices; YF-16 CCV aircraft; closed loop frequency; feedback control system; longitudinal aircraft control; model following strategy; multivariable frequency matching; transfer function matrix; Aircraft control; Multivariable systems; Output feedback; Position control; Transfer function matrices;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Applications, 1994., Proceedings of the Third IEEE Conference on
Conference_Location
Glasgow
Print_ISBN
0-7803-1872-2
Type
conf
DOI
10.1109/CCA.1994.381245
Filename
381245
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