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Output Feedback-Based Discrete-Time Sliding-Mode Controller Design for Model Aircraft

Chaudhuri, Anirban and Bhat, Seetharama M (2005) Output Feedback-Based Discrete-Time Sliding-Mode Controller Design for Model Aircraft. In: Journal of Guidance Control and Dynamics, 28 (1). pp. 177-181.

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Model aircraft provide a low-cost test bed for the design and validation of control algorithms. The control system should improve the transient response and have good disturbance-rejection properties. The stability derivatives of the aircraft vary due to in-flight velocity fluctuations and the controller should be invariant to such perturbations. Weight and power requirements of the aircraft payload restrict the number of onboard sensors and so a limited number of output measurements can be used for feedback.

Item Type: Journal Article
Additional Information: The copyright for this article belongs to American Institute of Aeronautics and Astronautics.
Keywords: Feedback-Based;Discrete-Time Sliding-Mode;Controller;Design;Model Aircraft
Department/Centre: Division of Mechanical Sciences > Aerospace Engineering(Formerly Aeronautical Engineering)
Depositing User: Ravi V Nandhan
Date Deposited: 25 Aug 2008
Last Modified: 19 Sep 2010 04:18
URI: http://eprints.iisc.ac.in/id/eprint/2800

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