Research Article
Recurrent Neural Network-Based Model Predictive Control for Multiple Unmanned Quadrotor Formation Flight
Table 2
Constraints of the system states and control inputs.
| | Parameters | Value |
| | Range of roll angle (rad) | | | Range of pitch angle (rad) | | | Range of yaw angle (rad) | | | Range of turn rates , , and (rad/s) | | | Range of the main thrust (N) | | | Range of the torque (M) | | | Range of the torque (M) | | | Range of the torque (M) | |
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