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dc.contributor.advisorArena, Andrew S.
dc.contributor.authorQuisenberry, Johnny Earl J., Jr.
dc.date.accessioned2014-04-17T19:53:40Z
dc.date.available2014-04-17T19:53:40Z
dc.date.issued2005-07-01
dc.identifier.urihttps://hdl.handle.net/11244/10031
dc.description.abstractThe goal of this paper is to produce a mathematical simulation of the aerial tow system with emphasis on low altitude tracking. The aerial tow system consists of a host aircraft which tows a smaller aircraft via cable. The system components are modeled and a method for deriving the system equations of motion in two and three-dimensional space is presented. The implementation of the system equations of motion in conjunction with a numerical solver results in the development of system simulation. The simulation is used as a tool to inspect various flight cases to better understand the nuances of the complex system.
dc.formatapplication/pdf
dc.languageen_US
dc.publisherOklahoma State University
dc.rightsCopyright is held by the author who has granted the Oklahoma State University Library the non-exclusive right to share this material in its institutional repository. Contact Digital Library Services at lib-dls@okstate.edu or 405-744-9161 for the permission policy on the use, reproduction or distribution of this material.
dc.titleDynamic Simulation of Low Altitude Aerial Tow Systems
dc.typetext
osu.filenameQuisenberryJr_okstate_0664M_1388.pdf
osu.collegeEngineering, Architecture, and Technology
osu.accesstypeOpen Access
dc.description.departmentMechanical & Aerospace Engineering
dc.type.genreThesis


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