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Experimental results on adaptive output feedback control using a laboratory model helicopter
Date
2002-01-01
Author
Kutay, Ali Türker
Idan, Moshe
Hovakimyan, Naira
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Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
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Experimental results are presented that illustrate a recently developed method for direct output feedback adaptive control. The method permits adaptation to both parametric uncertainty and unmodeled dynamics, and incorporates a novel approach that permits adaptation during periods of control saturation. A controller designed using this method was tested in controlling the pitch axis of a three degrees of freedom helicopter model, using attitude feedback through a low resolution optical sensor. © 2002 by the author(s).
URI
https://hdl.handle.net/11511/57054
DOI
https://doi.org/10.2514/6.2002-4921
Collections
Department of Aerospace Engineering, Conference / Seminar
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A. T. Kutay, M. Idan, and N. Hovakimyan, “Experimental results on adaptive output feedback control using a laboratory model helicopter,” 2002, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/57054.