Improved Aerodynamic Performance of Ornithopter Aerial Robot Using Spatial Mechanism Compared to Planar Design
Author:
Affiliation:
1. K. N. Toosi University of Technology,Center of Excellence in Robotics and Control, Advanced Robotics and Automated Systems (ARAS) Lab,Department of Mechanical Engineering,Tehran,Iran
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10412246/10412347/10412601.pdf?arnumber=10412601
Reference16 articles.
1. Flight; The Complete History of Aviation;Grant,1953
2. Integrated Product and Process Design for a Flapping Wing Drive Mechanism
3. Design of an active flapping wing mechanism and a micro aerial vehicle using a rotary actuator
4. Design of planar four-bar linkage with n specified positions for a flapping wing robot
5. Folding in and out: passive morphing in flapping wings
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