Method for multi unmanned aerial vehicle distributed formation control
A multi-UAV, UAV technology, applied in the direction of non-electric variable control, control/regulation system, three-dimensional position/channel control, etc.
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[0053] In a horizontal plane with a horizontal height of 5 meters, deploy 5 quadrotor UAVs (self-made quadrotor based on the open source flight control pixhawk, model: wheelbase 550mm). The hardware system of the UAV is mainly divided into the bottom flight control part and the upper computer part. The flight control part controls the flight stability of the drone, and the upper host computer is responsible for the specific algorithm control, and sends the calculated control speed to the bottom flight controller, so as to realize the autonomous flight of the drone.
[0054] The UAV can actively measure the relative position information of the neighbor UAV, mainly through the built-in laser scanner, can actively measure the relative position information of the neighbor UAV and itself, and convert the polar coordinates into the vector required by the algorithm.
[0055] The dynamic model of the motion of the UAV in the horizontal plane is as follows:
[0056] z' i =v i ,i=1,2...
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