Skip to main content

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