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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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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Citation Formats

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.