Flapping wing miniature aerial vehicles (FWMAVs) offer advantages over traditional fixed wing or quadrotor MAV platforms because they are more maneuverable than fixed wing aircraft and are more energy efficient than quadrotors, while being quieter than both. Currently, autonomy in FWMAVs has only been implemented in flapping vehicles without independent wing control, limiting their level of control. We have developed Robo Raven IV, a FWMAV platform with independently controllable wings and an actuated tail controlled by an onboard autopilot system. In this paper, we present the details of Robo Raven IV platform along with a control algorithm that uses a GPS, gyroscope, compass, and custom PID controller to autonomously loiter about a predefined point. We show through simulation that this system has the ability to loiter in a 50 meter radius around a predefined location through the manipulation of the wings and tail. A simulation of the algorithm using characterized GPS and tail response error via a PID controller is also developed. Flight testing of Robo Raven IV demonstrated the success of this platform, even in winds of up to 10 mph.
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ASME 2014 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference
August 17–20, 2014
Buffalo, New York, USA
Conference Sponsors:
- Design Engineering Division
- Computers and Information in Engineering Division
ISBN:
978-0-7918-4636-0
PROCEEDINGS PAPER
Autonomous Loitering Control for a Flapping Wing Miniature Aerial Vehicle With Independent Wing Control
Luke Roberts,
Luke Roberts
University of Maryland, College Park, MD
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Hugh A. Bruck,
Hugh A. Bruck
University of Maryland, College Park, MD
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Satyandra K. Gupta
Satyandra K. Gupta
University of Maryland, College Park, MD
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Luke Roberts
University of Maryland, College Park, MD
Hugh A. Bruck
University of Maryland, College Park, MD
Satyandra K. Gupta
University of Maryland, College Park, MD
Paper No:
DETC2014-34752, V05AT08A013; 10 pages
Published Online:
January 13, 2015
Citation
Roberts, L, Bruck, HA, & Gupta, SK. "Autonomous Loitering Control for a Flapping Wing Miniature Aerial Vehicle With Independent Wing Control." Proceedings of the ASME 2014 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. Volume 5A: 38th Mechanisms and Robotics Conference. Buffalo, New York, USA. August 17–20, 2014. V05AT08A013. ASME. https://doi.org/10.1115/DETC2014-34752
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