A robust adaptive control system for high performance aircraft / Tiauw Hiong Go

UNSPECIFIED (2009) A robust adaptive control system for high performance aircraft / Tiauw Hiong Go. Journal of Mechanical Engineering, 6 (1). pp. 67-84. ISSN 1823-5514

[img] Text
AJ_TIAUW HIONG GO JME 09.pdf

Download (0B)

Abstract

The design of a longitudinal controller to enhance the maneuverability of a high performance aircraft is described. Since such aircraft is often required to fly outside the linear aerodynamic regimes, the design is based on the nonlinear equations of motion. The controller is of adaptive type and it is robust with respect to unknown, but bounded uncertainties. The performance of the resulting controller is evaluated through simulations using hypothetical fighter aircraft parameters. The controller is demonstrated to be able to obtain good and consistent performances over a wide range of flight conditions.

Item Type: Article
Divisions: Faculty of Mechanical Engineering
Journal or Publication Title: Journal of Mechanical Engineering
ISSN: 1823-5514
Volume: 6
Number: 1
Page Range: pp. 67-84
Item ID: 17621
Uncontrolled Keywords: A robust adaptive control system; Aircraft
Last Modified: 17 Aug 2017 03:37
Depositing User: Staf Pendigitalan 5
URI: http://ir.uitm.edu.my/id/eprint/17621

Actions (login required)

View Item View Item

Downloads

Downloads per month over past year