Research Article
Real-Time Hovering Control of Unmanned Aerial Vehicles
| | Mass of the airframe | 1.1 kg |
| | Distance of the center of mass to the rotor shaft | 0.223 m | | Inertia in the -axis | 6.825 kg | | Inertia in the -axis | 6.825 kg | | Inertia in the -axis | 12.39 kg | | Inertia of the propellers | 6 kg | | Gravity acceleration | 9.81 m/ | | Thrust factor | 54.2 | | Drag factor | 1.1 N | | Roll angle | deg | | Pitch angle | deg | | Yaw angle | deg | | -position | m |
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