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Table 6 Non-dimensional aerodynamic derivatives

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