From: Aerodynamics and dynamic stability of micro-air-vehicle with four flapping wings in hovering flight
Xu+ | Xw+ | Xq+ | Zu+ | Zw+ | Zq+ | Mu+ | Mw+ | Mq+ |
---|---|---|---|---|---|---|---|---|
− 1.421 | 0 | 0 | −0.059 | −1.25 | 0 | 0.059 | 0 | −0.014 |
\( {}_{Y_v^{+}} \) | \( {Y}_p^{+} \) | \( {Y}_r^{+} \) | \( {L}_v^{+} \) | \( {L}_p^{+} \) | \( {L}_r^{+} \) | \( {N}_v^{+} \) | \( {N}_p^{+} \) | \( {N}_r^{+} \) |
− 1.025 | − 0.1 | 0 | −0.112 | − 0.385 | 0 | 0 | 0 | −1.525 |