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

Volume

2

fYear

2006

fDate

Aug. 30 2006-Sept. 1 2006

Firstpage

150

Lastpage

153

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;

fLanguage

English

Publisher

ieee

Conference_Titel

Innovative Computing, Information and Control, 2006. ICICIC '06. First International Conference on

Conference_Location

Beijing

Print_ISBN

0-7695-2616-0

Type

conf

DOI

10.1109/ICICIC.2006.254

Filename

1691950