Research Article
Modeling and Analysis of Chaos and Bifurcations for the Attitude System of a Quadrotor Unmanned Aerial Vehicle
Table 2
Parameter values of the quadrotor [
3,
8].
| Parameter | Value |
| (m/s2) | 9.81 | (kg) | 0.468 | (m) | 0.225 | (N·m/rad/s) | 2.9e − 5 | (m) | 1.1e − 6 | (kg·m2) | 3.4e − 5 | Ix (kg·m2) | 4.9e − 3 | Iy (kg·m2) | 9.8e − 3 | Iz (kg·m2) | 8.8e − 3 | (N/m/s) | 2.45e − 4 | (N/m/s) | 8.82e − 4 | (N/m/s) | 4.40e − 4 | (N/rad/s) | 2.45e − 4 | (N/rad/s) | 8.82e − 4 | (N/rad/s) | 4.40e − 4 |
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