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This document is the culmination of research into small unmanned Powered Parachute aerial vehicles. This dissertation serves to provide designers of small systems with an approach to developing a Powered Parachute Unmanned Aerial Vehicle system, guiding them through the basic assumptions, dynamics, and control method.

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    Date Created
    2022
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  • Text
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    • Partial requirement for: Ph.D., Arizona State University, 2022
    • Field of study: Engineering

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