Abstract
Aerial robotic platforms are an increasingly sought-after solution for a variety of sensing, monitoring, and transportation challenges. However, as invaluable as unmanned aerial vehicles (UAVs) have been for these applications, fixed-wing and multi-rotor systems each have individual limitations. Fixed-wing UAVs are generally capable of high-altitude surveillance and long flight times, while quad-rotors are most effective when used for their maneuverability and close-quarters surveying. This paper improves upon the prototypes discussed in [1] by creating a series of three next-generation prototypes to isolate the aspects of solar powered fixed-wing flight, quad-rotor flight, and transformation modes of the SUAV:Q platform. Improvements to the transformation mechanism, airframe design, variable pitch propulsion system, and custom-designed power electronics are presented along with validation of the designs through empirical testing.
Original language | English (US) |
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Title of host publication | ICRA 2017 - IEEE International Conference on Robotics and Automation |
Publisher | Institute of Electrical and Electronics Engineers Inc. |
Pages | 3917-3923 |
Number of pages | 7 |
ISBN (Electronic) | 9781509046331 |
DOIs | |
State | Published - Jul 21 2017 |
Event | 2017 IEEE International Conference on Robotics and Automation, ICRA 2017 - Singapore, Singapore Duration: May 29 2017 → Jun 3 2017 |
Publication series
Name | Proceedings - IEEE International Conference on Robotics and Automation |
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ISSN (Print) | 1050-4729 |
Other
Other | 2017 IEEE International Conference on Robotics and Automation, ICRA 2017 |
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Country/Territory | Singapore |
City | Singapore |
Period | 5/29/17 → 6/3/17 |
Bibliographical note
Funding Information:This material is based upon work supported by the National Science Foundation through grants #CNS-0934327, #CNS-1439728, #IIS-1427014, #OISE-1551059, #CNS-1531330, and #CNS-1544887. Ruben DSa was supported by a National Science Foundation Graduate Research Fellowship No. 00039202.