DocumentCode
1246292
Title
A robustly stable preliminary control systems design for the YF-16 CCV aircraft
Author
Pujara, L.R.
Author_Institution
Dept. of Electr. Eng., Wright State Univ., Dayton, OH, USA
Volume
31
Issue
1
fYear
1995
Firstpage
479
Lastpage
486
Abstract
A preliminary control system design for the YF-16 CCV aircraft in its longitudinal mode satisfying its flying qualities specifications is investigated. The design is shown to be robustly stable when the actuator model and the unstable pole in the airframe model of the aircraft are subjected to structured uncertainties. Very recent tools of robust stability analysis are utilized to accomplish this goal.<>
Keywords
actuators; aircraft control; approximation theory; control system synthesis; poles and zeros; polynomials; robust control; YF-16 CCV aircraft; actuator model; airframe model; longitudinal mode; preliminary control systems; robust stability; structured uncertainties; unstable pole; Actuators; Aerospace control; Aircraft; Control design; Control systems; Robust control; Robust stability; Robustness; Transfer functions; Uncertainty;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/7.366331
Filename
366331
Link To Document