Skip to main content

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°)