Description
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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Contributors
- Fiedler, Brett (Author)
- Redkar, Sangram (Thesis advisor)
- Sugar, Thomas (Committee member)
- Phatak, Amar (Committee member)
- Arizona State University (Publisher)
Date Created
The date the item was original created (prior to any relationship with the ASU Digital Repositories.)
2022
Resource Type
Collections this item is in
Note
- Partial requirement for: Ph.D., Arizona State University, 2022
- Field of study: Engineering