Description
This thesis project examines the stability margin for different rotor configurations for a quadcopter and compares them against each other to determine the most stable flight configuration possible. The first configuration develops a “standard” for quadcopters with each motor in a corner of a cube at a 60-degree angle from the Y-Axis.
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Contributors
- Corino, Tyler Michael (Author)
- Kuo, Chen-Yuan (Thesis director)
- Lynch, John (Committee member)
- Mechanical and Aerospace Engineering Program (Contributor)
- Barrett, The Honors College (Contributor)
Date Created
The date the item was original created (prior to any relationship with the ASU Digital Repositories.)
2020-05
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