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)|
|Date Deposited:||25 Aug 2008|
|Last Modified:||19 Sep 2010 04:18|
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