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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