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dc.contributor.advisorTischler, Mark B.
dc.contributor.advisorWood, E.R.
dc.contributor.authorLabows, Steven J.
dc.date.accessioned2013-05-08T20:44:03Z
dc.date.available2013-05-08T20:44:03Z
dc.date.issued2000-03
dc.identifier.urihttp://hdl.handle.net/10945/32950
dc.description.abstractHelicopters operate in an environment where task performance can easily be affected by atmospheric turbulence. This paper discusses the airborne flight test of the Sikorsky UH-60 Black Hawk helicopter in turbulent conditions to determine disturbance rejection criteria and to develop a low speed turbulence model for helicopter simulation. A simple approach to modeling the aircraft response to turbulence is described by using an identified model of the Black Hawk to extract representative control inputs that replicate the aircraft response to disturbances. This parametric turbulence model is designed to be scaled for varying levels of turbulence and utilized in ground or in-flight simulation. Flight control cutoff frequency data are also analyzed to support design criteria for gust rejection handling qualitiesen_US
dc.description.urihttp://archive.org/details/uhblackhawkdistu1094532950
dc.format.extentxiv, 108 p.;28 cm.en_US
dc.language.isoen_US
dc.publisherMonterey, California. Naval Postgraduate Schoolen_US
dc.subject.lcshNAen_US
dc.titleUH-60 Black Hawk disturbance rejection study for hover/low speed handling qualities criteria and turbulence modelingen_US
dc.title.alternativeNAen_US
dc.typeThesisen_US
dc.contributor.secondreaderNA
dc.contributor.departmentAeronautical Engineering
dc.subject.authorNAen_US
dc.description.funderNAen_US
dc.description.recognitionNAen_US
dc.description.serviceU.S. Navy (U.S.N.) author.en_US
etd.thesisdegree.nameM.S. in Aeronautical Engineeringen_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.disciplineAeronautical Engineeringen_US
etd.thesisdegree.grantorNaval Postgraduate Schoolen_US
dc.description.distributionstatementApproved for public release; distribution is unlimited.


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