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Flight controller design via combined sliding mode and linear state-feedback technique

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2 Author(s)
Chen, Y.P. ; Inst. of Control Eng., Nat. Chiao Tung Univ., Hsinchu, Taiwan ; Yu, J.R.

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.<>

Published in:

TENCON '93. Proceedings. Computer, Communication, Control and Power Engineering.1993 IEEE Region 10 Conference on  (Volume:4 )

Date of Conference:

19-21 Oct. 1993