Title :
Flight controller design via combined sliding mode and linear state-feedback technique
Author :
Chen, Y.P. ; Yu, J.R.
Author_Institution :
Inst. of Control Eng., Nat. Chiao Tung Univ., Hsinchu, Taiwan
Abstract :
This paper presents the design of an aircraft flight controller. A plant with mismatched perturbation around its nominal system is considered. To cope with such a problem, a new combined scheme which adopts both the sliding-mode and the linear state-feedback techniques is presented. An example is included to show the success of the control algorithms.<>
Keywords :
aircraft control; control system synthesis; matrix algebra; state feedback; variable structure systems; aircraft flight controller; design; linear state-feedback; matrix algebra; mismatched perturbation; sliding mode control; Aerodynamics; Aerospace control; Aerospace electronics; Aircraft; Control systems; Mathematical model; Motion control; Nonlinear dynamical systems; Nonlinear equations; Sliding mode control;
Conference_Titel :
TENCON '93. Proceedings. Computer, Communication, Control and Power Engineering.1993 IEEE Region 10 Conference on
Conference_Location :
Beijing, China
Print_ISBN :
0-7803-1233-3
DOI :
10.1109/TENCON.1993.320508
