A ROBUSTLY STABLE PRELIMINARY CONTROL-SYSTEMS DESIGN FOR THE YF-16 CCV AIRCRAFT

Authors
PUJARA LR
Citation
Lr. Pujara, A ROBUSTLY STABLE PRELIMINARY CONTROL-SYSTEMS DESIGN FOR THE YF-16 CCV AIRCRAFT, IEEE transactions on aerospace and electronic systems, 31(1), 1995, pp. 479-486
Citations number
8
Categorie Soggetti
Telecommunications,"Engineering, Eletrical & Electronic","Aerospace Engineering & Tecnology
Journal title
IEEE transactions on aerospace and electronic systems → ACNP
ISSN journal
00189251
Volume
31
Issue
1
Year of publication
1995
Pages
479 - 486
Database
ISI
SICI code
0018-9251(1995)31:1<479:ARSPCD>2.0.ZU;2-N
Abstract
A preliminary control system design for the YF-16 CCV aircraft in its longitudinal mode satisfying its flying qualities specifications is in vestigated 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 st ability analysis are utilized to accomplish this goal.