Modeling and Simulation of Nonlinear Dynamics of Flapping Wing Micro Air Vehicles
Author:
Affiliation:
1. University of Michigan, Ann Arbor, Michigan 48109
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J050649
Reference41 articles.
1. Dynamic flight stability in the desert locustSchistocerca gregaria
2. The mechanics of flight in the hawkmoth Manduca sexta. I. Kinematics of hovering and forward flight.
3. The aerodynamics of hovering insect flight. I. The quasi-steady analysis
4. Dragonfly flight. I. Gliding flight and steady-state aerodynamic forces.
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