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Control, Propulsion and Energy Assessment of a Spherical UAS for Low Speed Operations Independent researcher
- Format:
- Conference/Event
- Author/Creator:
- Bandycki, Bandycki, author.
- Conference Name:
- Aerospace Technology Conference & Exposition (2017-09-26 : Fort Worth, Texas, United States)
- Language:
- English
- Physical Description:
- 1 online resource
- Place of Publication:
- Warrendale, PA SAE International 2017
- Summary:
- AbstractThis paper presents a comparison between different hypotheses of propulsion of a spherical UAS. Different architectures have been analyzed assessing their specific aerodynamic, energetic, and flight mechanics features. The comparison has been performed assuming the robustness of flight control in different wind conditions, defining for each the specific operative ranges, mission profiles, and energy assessment. An effective energy assessment and comparison against a commercial UAS has been produced. Even if the paper considers a preliminary simplified configuration, it demonstrates clearly to be competitive against traditional quadcopters in a predefined reference mission
- Notes:
- Vendor supplied data
- Publisher Number:
- 2017-01-2065
- Access Restriction:
- Restricted for use by site license
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