Research Article
Design and Simulation of Eight-Rotor Unmanned Aerial Vehicle Based on Hybrid Control System
Table 1
Main parameters of UAV model.
| | Parameter | Value | Parameter | Value |
| | Quality () | 1.9 | Rotor’s length () | 0.32 | | Lift coefficient | 3.13 | Resistance coefficient | 7.5 | | -axis rotary inertia | 0.018 | -axis rotary inertia | 0.018 | | -axis rotary inertia | 0.036 | Gravitational acceleration () | 9.8 |
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