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dc.contributor.advisorWood, E.R.
dc.contributor.authorWagner, Roy C.
dc.dateSeptember 1995
dc.date.accessioned2012-07-31T19:55:03Z
dc.date.available2012-07-31T19:55:03Z
dc.date.issued1995-09
dc.identifier.urihttps://hdl.handle.net/10945/7596
dc.description.abstractThis thesis uses Flightlab to model and analyze the flight dynamics of the SH-6OB Seahawk helicopter. Flightlab runs on computers utilizing the UNIX operating system and is used for design, analysis and testing of an aircraft using non-linear modeling techniques. It is capable of modeling conventional main rotor-tail rotor and tandem rotor helicopters and tilt rotor aircraft. A procedural guide for modeling and analyzing a single main rotor helicopter is presented using the SH-60B. The non-linear response from lateral and longitudinal cyclic, main rotor collective and tail rotor collective inputs are presented. Flightlab is also capable of reducing the non-linear model to a linear model. The linear and non-linear models are then compared. The purpose of this thesis is to present a guide for using Flightlab to model and analyze an existing helicopter design, and also to have in place a well tested model to be used for further research.en_US
dc.description.urihttp://archive.org/details/proceduralguidef109457596
dc.format.extent168 p.en_US
dc.language.isoen_US
dc.publisherMonterey, California. Naval Postgraduate Schoolen_US
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.en_US
dc.titleProcedural guide for modeling and analyzing the flight dynamics of the SH-60B helicopter using Flightlaben_US
dc.typeThesisen_US
dc.contributor.departmentAeronautical Engineering
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


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