Table 9 Eigenvectors of the system matrix
From: Aerodynamics and dynamic stability of micro-air-vehicle with four flapping wings in hovering flight
δu+ | δw+ | δq+ | δθ+ | |
|---|---|---|---|---|
Longitude mode 1 | 0.714(124.77°) | 0.015(246.61°) | 0.082(84.80°) | 1(0°) |
Longitude mode 2 | 0.677(0°) | 0.012(0°) | 0.153(180°) | 1(0°) |
Longitude mode 3 | 0 | 1 | 0 | 0 |
δv+ | δp+ | δr+ | δϕ+ | |
Lateral mode 1 | 0.392 (− 58.55°) | 0.112(73.08°) | 0 | 1(0°) |
Lateral mode 2 | 0 | 0 | 1 | 0 |
Lateral mode 3 | 0.393(180°) | 0.162(180°) | 0 | 1(0°) |