From: Aerodynamics and dynamic stability of micro-air-vehicle with four flapping wings in hovering flight
Mode1 | Mode2 | Mode3 | |
---|---|---|---|
BB | −0.12 ± 0.07i | −0.69 | 0.09 |
DF | −0.09 ± 0.06i | −0.51 | 0.08 |
HM | −0.57 ± 0.26i | −5.68 | 0.26 |
Four-winged FMAV | 0.0326 ± 0.1072i | −0.654 | −0.162 |