Cart (Loading....) | Create Account
Close category search window
 

Free flight simulations and pitch and roll control experiments of a sub-gram flapping-flight micro aerial vehicle

Sign In

Cookies must be enabled to login.After enabling cookies , please use refresh or reload or ctrl+f5 on the browser for the login options.

Formats Non-Member Member
$31 $13
Learn how you can qualify for the best price for this item!
Become an IEEE Member or Subscribe to
IEEE Xplore for exclusive pricing!
close button

puzzle piece

IEEE membership options for an individual and IEEE Xplore subscriptions for an organization offer the most affordable access to essential journal articles, conference papers, standards, eBooks, and eLearning courses.

Learn more about:

IEEE membership

IEEE Xplore subscriptions

3 Author(s)
Hines, L.L. ; Robot. Inst., Carnegie Mellon Univ., Pittsburgh, PA, USA ; Arabagi, V. ; Sitti, M.

Flapping-flight micro aerial vehicles (MAVs) pose an ongoing design problem to the scientific community, requiring careful consideration of both body structure and force production. Here, we examine a flapping MAV prototype with a passively rotating wing design. While at the current scale the lift force produced is not enough for liftoff, observing its performance under roll and pitch control can lead to insights on both the body design and the eventual free-flight implementation. As the production of roll and pitch torques are primarily uncoupled for this design, PID control is implemented in the roll and pitch directions individually on a custom designed single degree of freedom rig. By doing so, we show that the body structure is capable of sustaining independent wing amplitudes and that actuator input voltage bias shifting is successful experimentally on a dynamically driven wing. Through force compensation, the experimentally tested controller is mapped to a 1/2 scale simulated system, theoretically capable of free-flight. Though initial simulation results suggest high sensitivity to feedback noise, simulations show that decoupled roll and pitch controllers have potential as a minimal computational means for hovering and translational motion.

Published in:

Robotics and Automation (ICRA), 2011 IEEE International Conference on

Date of Conference:

9-13 May 2011

Need Help?


IEEE Advancing Technology for Humanity About IEEE Xplore | Contact | Help | Terms of Use | Nondiscrimination Policy | Site Map | Privacy & Opting Out of Cookies

A not-for-profit organization, IEEE is the world's largest professional association for the advancement of technology.
© Copyright 2014 IEEE - All rights reserved. Use of this web site signifies your agreement to the terms and conditions.