From: Aerodynamics and dynamic stability of micro-air-vehicle with four flapping wings in hovering flight
Longitudinal Mode 1 | Longitudinal Mode 2 | Longitudinal Mode 3 |
---|---|---|
0.0074 ± 0.0811i | −0.153 | − 0.043 |
Lateral Mode 1 | Lateral Mode 2 | Lateral Mode 3 |
0.0326 ± 0.1072i | −0.654 | − 0.162 |