Coupled Unsteady Aero-Flight Dynamics of Hovering Insects/Flapping Micro Air Vehicles
Author:
Affiliation:
1. University of California, Irvine, California 92697
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034205
Reference48 articles.
1. Wing Rotation and the Aerodynamic Basis of Insect Flight
2. Effect of the aerodynamic-induced parametric excitation on the longitudinal stability of hovering MAVs/insects
3. Stability in Ornithopter Longitudinal Flight Dynamics
4. Wingbeat Shape Modulation for Flapping-Wing Micro-Air-Vehicle Control During Hover
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