Title :
Control Design for Longitudinal Flight Dynamics
Author :
Liaw, Der-Cherng ; Chung, Wen-Ching ; Hsieh, Chien-Shu
Author_Institution :
Dept. of Electr. & Control Eng., Nat. Chiao Tung Univ., Hsinchu
fDate :
Aug. 30 2006-Sept. 1 2006
Abstract :
In this paper, the control issues of longitudinal flight dynamics is presented. System controllability with respect to the variation of the elevator deflection angle is first discussed. Stabilization controllers using washout filter-aided feedback control law is then proposed. Case study for F-8 aircraft is explicitly derived for constructing a feasible set of controllers. Numerical simulations for bifurcation scenarios are also given to compare the performance of the designs
Keywords :
aerodynamics; aircraft control; control system synthesis; controllability; feedback; stability; F-8 aircraft; bifurcation scenario; control design; elevator deflection angle variation; longitudinal flight dynamics; stabilization controller; system controllability; washout filter-aided feedback control law; Aerospace control; Aircraft manufacture; Bifurcation; Control design; Control systems; Controllability; Elevators; Feedback control; Numerical simulation; Optimal control;
Conference_Titel :
Innovative Computing, Information and Control, 2006. ICICIC '06. First International Conference on
Conference_Location :
Beijing
Print_ISBN :
0-7695-2616-0
DOI :
10.1109/ICICIC.2006.254
