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Dynamics of Flapping Micro-Aerial Vehicles
| Content Provider | CiteSeerX |
|---|---|
| Author | Yang, T. M. Hsiao, F. Y. |
| Abstract | for several years. Based on the developed flapping-wing MAVs we study its dynamics and compare our results with flight test data. Although several papers have discussed similar topics previously, using our flight test data we demonstrate the validity of the assumptions and derivations. We also propose a claim that links the average aerodynamical forces to the wind tunnel test data, so that a flapping MAV can be analyzed with the same methodology as what we have done to a fixed-wing aircraft. Flight test data and numerical simulations are also provided to demonstrate the validity of our derivation. I. |
| File Format | |
| Access Restriction | Open |
| Subject Keyword | Flight Test Data Micro-aerial Vehicle Several Year Similar Topic Fixed-wing Aircraft Average Aerodynamical Force Wind Tunnel Test Data Several Paper Numerical Simulation Developed Flapping-wing Mavs |
| Content Type | Text |
