Experimental results on adaptive output feedback control using a laboratory model helicopter

Date

2005-03-01

Author

Kutay, Ali Türker
Idan, M
Hovakimyan, N

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Experimental results are presented that illustrate a recently developed method for adaptive output feedback control. The method permits adaptation to both parametric uncertainty and unmodeled dynamics, and incorporates a novel approach that permits adaptation under known actuator characteristics including actuator dynamics and saturation. Only knowledge of the relative degree of the controlled system within the bandwidth of the control design is required. The controller design was tested by controlling the pitch axis of a three degrees-of-freedom (DOF) helicopter model, using attitude feedback through a low-resolution optical sensor.

Subject Keywords

Control and Systems Engineering, Electrical and Electronic Engineering

URI

https://hdl.handle.net/11511/56866

Journal

IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY

DOI

https://doi.org/10.1109/tcst.2004.839563

Collections

Department of Aerospace Engineering, Article

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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,” IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, pp. 196–202, 2005, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/56866.