Title :
A robustly stable preliminary control systems design for the YF-16 CCV aircraft
Author_Institution :
Dept. of Electr. Eng., Wright State Univ., Dayton, OH, USA
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;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
