@inproceedings{a83fab0613334e7595ddeddab89c513c,
title = "Experimental results on adaptive output feedback control using a laboratory model helicopter",
abstract = "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.",
author = "Kutay, {Ali T.} and Calise, {Anthony J.} and Moshe Idan and Naira Hovakimyan",
year = "2002",
doi = "10.2514/6.2002-4921",
language = "English (US)",
isbn = "9781563479786",
series = "AIAA Guidance, Navigation, and Control Conference and Exhibit",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
booktitle = "AIAA Guidance, Navigation, and Control Conference and Exhibit",
note = "AIAA Guidance, Navigation, and Control Conference and Exhibit 2002 ; Conference date: 05-08-2002 Through 08-08-2002",
}