A formation tracking control method for quadrotor aircraft
A four-rotor aircraft and tracking control technology, applied in the field of UAV, can solve the problems of complex dynamics, influence of convergence time, anti-interference and robustness to be improved, and achieve less calculation, reduce coupling, and strong robustness The effect of stickiness and noise immunity
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[0048] like figure 1 As shown, the specific implementation of the multi-UAV formation control method based on the fixed time consistency theory proposed by the present invention is as follows:
[0049] Take 3 UAVs as an example and a virtual leader as an example, set the total flight time to 15 seconds, and observe whether the UAVs form the desired formation and the time to form the formation.
[0050] Step 1: Give the quadrotor UAV dynamics model, the specific steps are as follows:
[0051] The four inputs of the drone are generated by the four rotors, and the four rotor pulling forces and three axial moments are obtained, and the combined pulling force of the four rotors is T i , the torque is τ φ,i is the rolling moment, τ θ,i is the pitching moment, τ ψ,i For the yaw moment, the moment imbalance is the reason for the rotational motion of the drone. If the rotational speeds of the four rotors are respectively w 1,i , w 2,i , w 3,i , w 4,i ,Available
[0052] ...
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