Research Article
Control of a Tilting Hexacopter under Wind Disturbance
| | Parameters | Value | Unit |
| | Hexacopter’s mass, | 2.274 | kg | | Gravitational acceleration, | 9.81 | | | Inertia tensor in the x-axis, Ixx | 0.516 | | | Inertia tensor in the y-axis, Iyy | 0.516 | | | Inertia tensor in the z-axis, | 0.982 | | | Lift coefficient, | | — | | Resistance coefficient, | | — | | Moment of inertia in tilting axis, | | | | Gyro moment coefficient, | | | | Air density, | 1.293 | | | Average windward area, | 0.107 | | | Coefficient of air resistance, | 0.08 | — |
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