Design and testing of flapping wing control for a micro air vehicle

Authors

Michael L. Anderson, Air Force Institute of Technology

Document Type

Conference Proceeding

Publication Date

8-11-2011

Department

Department of Aeronautics and Astronautics

School or Division

Graduate School of Engineering and Management

Digital Object Identifier

10.2514/6.2011-6226

Source Publication

AIAA Guidance, Navigation and Control Conference 2011

Comments

This conference paper is available to AIAA subscribers through the DOI link on this page.

Author Michael Anderson was an AFIT PhD candidate at the time of this conference. (AFIT-DS-ENY-11-12, September 2011).

Recommended Citation

Anderson, M. L. (2011). Design and testing of flapping wing control for a micro air vehicle. AIAA Guidance, Navigation and Control Conference 2011. https://doi.org/10.2514/6.2011-6226