Flapping wing unmanned aerial vehicles (FWUAVs) provide an alternative to traditional platforms because they are more maneuverable than fixed wing platforms while being faster, quieter, and more natural looking than rotary wing platforms. While real birds are able to execute complex and highly controlled aerobatic maneuvers, executing FWUAV aerobatics presents unique challenges due to difficulty in execution of controlled quick orientation change. This paper demonstrates a simple method for using a large 2 degree of freedom tail for quick orientation changes and flight control, enabling execution of a pre-programmed backflip maneuver on the Robo Raven V, a hybrid FWUAV. The platform reached angular velocities of up to 420° per second during the maneuver.
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ASME 2016 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference
August 21–24, 2016
Charlotte, North Carolina, USA
Conference Sponsors:
- Design Engineering Division
- Computers and Information in Engineering Division
ISBN:
978-0-7918-5015-2
PROCEEDINGS PAPER
Using a Large 2 Degree of Freedom Tail for Autonomous Aerobatics on a Flapping Wing Unmanned Aerial Vehicle
Luke Roberts,
Luke Roberts
University of Maryland College Park, College Park, MD
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Hugh Bruck,
Hugh Bruck
University of Maryland College Park, College Park, MD
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S. K. Gupta
S. K. Gupta
University of Southern California, Los Angeles, CA
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Luke Roberts
University of Maryland College Park, College Park, MD
Hugh Bruck
University of Maryland College Park, College Park, MD
S. K. Gupta
University of Southern California, Los Angeles, CA
Paper No:
DETC2016-60387, V05AT07A074; 11 pages
Published Online:
December 5, 2016
Citation
Roberts, L, Bruck, H, & Gupta, SK. "Using a Large 2 Degree of Freedom Tail for Autonomous Aerobatics on a Flapping Wing Unmanned Aerial Vehicle." Proceedings of the ASME 2016 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. Volume 5A: 40th Mechanisms and Robotics Conference. Charlotte, North Carolina, USA. August 21–24, 2016. V05AT07A074. ASME. https://doi.org/10.1115/DETC2016-60387
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