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dc.contributor.authorFoster, Nicholas
dc.contributor.authorUtley, Lucas
dc.contributor.authorWalsh, Andrew
dc.contributor.authorKadavy, Ben
dc.contributor.authorKenkel, Chad
dc.contributor.authorMcCullers, Gerald
dc.contributor.authorKunka, Logan
dc.contributor.authorGeorge, Nicholas
dc.contributor.authorRitchie, Caleb
dc.contributor.authorRosario, Jake
dc.date.accessioned2018-11-21T21:24:58Z
dc.date.available2018-11-21T21:24:58Z
dc.date.issued2018-05-02
dc.identifieroksd_kadavy_HT_2018
dc.identifier.urihttps://hdl.handle.net/11244/302116
dc.description.abstractThe goal of this project was to design and develop a rocket that could get a payload golf ball to at least 8,000 AGL and then return it as close to the X on the ground as possible. In order to achieve this goal, we decided to design an integrated deployable quadcopter UAC that would deploy at apogee and then autonomously fly itself back to the designated target location. This concept has never been achieved before and therefore we wanted to be the first to successfully complete the mission. Despite our work and determination we were unsuccessful of a true recovery however we believe we have made the most progress and had the most success of anyone attempting such a feat at the high-powered rocketry level.
dc.formatapplication/pdf
dc.languageen_US
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.titleRocket launched autonomous quadcopter final report
osu.filenameoksd_kadavy_HT_2018.pdf
osu.accesstypeOpen Access
dc.type.genreHonors Thesis
dc.type.materialText
thesis.degree.disciplineMechanical and Aerospace Engineering
thesis.degree.grantorOklahoma State University


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