Research Article
Online Adaptive Error Compensation SVM-Based Sliding Mode Control of an Unmanned Aerial Vehicle
Table 1
Quad-rotor parameters in simulation.
| | Parameter | Value |
| | 0.468 kg | | 9.81 m/s2 | | 0.225 m | | 2.98 × 10−6 N⋅s/rad2 | | 1.14 × 10−7 N⋅m⋅s/rad2 | | 4.856 × 10−3 kg⋅m2 | | 4.856 × 10−3 kg⋅m2 | | 8.801 × 10−3 kg⋅m2 | | 6.15 × 10−5 kg⋅m2 | | 6.15 × 10−5 kg⋅m2 |
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