Title :
Sliding mode control scheme for aircraft
Author :
Zhan-shan, Zhao ; Jing, Zhang ; Lian-kun, Sun ; Gang, Ding
Author_Institution :
Comput. Sci. & Software Instn., Tianjin Polytech. Univ., Tianjin, China
Abstract :
An Integral sliding mode based on the finite time stabilization control scheme for the longitudinal dynamics of aircraft is proposed in this paper. The Input/Output Linearization technique is applied for control design to linearize the dynamics of aircraft with respect to air speed V and altitude h. Simulation studies demonstrate that the proposed controller is robust with respect to the perturbation.
Keywords :
aircraft control; control system synthesis; stability; variable structure systems; aircraft; control design; finite time stabilization control; input/output linearization technique; integral sliding mode; longitudinal dynamics; sliding mode control; Aerospace control; Aircraft; Atmospheric modeling; Mathematical model; Robustness; Vehicle dynamics; Vehicles; Aircraft; Linearization technique; Sliding Mode Control; insert; styling;
Conference_Titel :
Computer and Information Application (ICCIA), 2010 International Conference on
Conference_Location :
Tianjin
Print_ISBN :
978-1-4244-8597-0
DOI :
10.1109/ICCIA.2010.6141591
