ePrints@IIScePrints@IISc Home | About | Browse | Latest Additions | Advanced Search | Contact | Help

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.

[img] PDF
getpdf.pdf
Restricted to Registered users only

Download (237Kb) | Request a copy

Abstract

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)
Date Deposited: 25 Aug 2008
Last Modified: 19 Sep 2010 04:18
URI: http://eprints.iisc.ernet.in/id/eprint/2800

Actions (login required)

View Item View Item