Research Article
Quadrotor Identification through the Cooperative Particle Swarm Optimization-Cuckoo Search Approach
Table 1
The parameters of the quadrotor.
| | Parameter | Definition | Value |
| | (kg·m2) | The inertia moments with respect to the axes | 7.5 · 10−3 | | (kg·m2) | 7.5 · 10−3 | | (kg·m2) | 1.3 · 10−3 |
| | (N/rad/s) | The aerodynamic coefficients | 5.567 · 10−4 | | (N/rad/s) | 5.567 · 10−4 | | (N/rad/s) | 6.354 · 10−4 |
| | (N/rad/s) | The drag coefficients | 5.567 · 10−4 | | (N/rad/s) | 5.567 · 10−4 | | (N/rad/S) | 6.354 · 10−4 |
| | (m/s) | The gravity acceleration | 9.806 | | (kg·m2) | The inertia of the rotors | 2.8385 · 10−5 | | b (kg·m·rad−2) | The thrust coefficient | 2.9842 · 10−5 | | d (kg·m·rad−2) | The drag coefficient | 3.232 · 10−6 | | m (kg) | The total mass of the quadrotor | 0.65 | | l (m) | The half span of the quadrotor | 0.23 |
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