Integration of an Autopilot for a Micro Air Vehicle

Author:

Platanitis George1,Shkarayev Sergey1

Affiliation:

1. University of Arizona

Publisher

American Institute of Aeronautics and Astronautics

Reference26 articles.

1. Effect of Camber on the Aerodynamics of Adaptive Wing Micro Air Vehicles

2. Shkarayev, S., Null, W., and Wagner, M. "Development of Micro Air Vehicle Technology with In-Flight adaptive-WingStructure," NASA/CR-2004-213271, October2004.

3. Null, W. "The Design and Development of an Adaptive Wing Micro Air Vehicle," M.S. thesis,University of Arizona, 2003.

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