Comparison of Yaw Moment Generation Methods for Motor Directly Driven Flapping Wing Micro Aerial Vehicle
Author:
Affiliation:
1. Konkuk University,Department of Smart Vehicle Engineering,Seoul,Korea,05029
2. Konkuk University,Department of Mechanical and Aerospace Engineering,Seoul,Korea,05029
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10316683/10316739/10316936.pdf?arnumber=10316936
Reference8 articles.
1. Model-Based Evaluation of Control Roll, Pitch, Yaw Moments for a Robotic Hummingbird
2. Wingbeat Shape Modulation for Flapping-Wing Micro-Air-Vehicle Control During Hover
3. KUBeetle-S: An insect-like, tailless, hover-capable robot that can fly with a low-torque control mechanism
4. Tailless Insect-Mimicking Flapping-Wing Micro Air Vehicle: A Review and Perspective
5. Resonance Principle for the Design of Flapping Wing Micro Air Vehicles
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