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Table 7 Eigenvalues of system matrix

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