Research Article
U-Model-Based Sliding Mode Controller Design for Quadrotor UAV Control Systems
Table 1
Quadrotor parameters [
14].
| | Parameters | Values |
| | m (kg) | 1.2 | | l (m) | 0.2 | | kt × 10−5 (N·s2) | 3.13 | | kd × 10−7 (N·s2) | 7.5 | | Ix × 10−3 (kg·m2) | 2.353 | | Iy × 10−7 (kg·m2) | 2.353 | | Iz × 10−7 (kg·m2) | 5.262 |
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