High-precision unmanned aerial vehicle flight control system
A flight control system and UAV technology, applied in aircraft, information technology support systems, motor vehicles, etc., can solve problems such as unmanned aerial vehicles cannot be charged, UAV inspection radius restrictions, etc., to increase the voyage and inspection radius, The effect of reducing my time cost and labor cost
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Embodiment 1
[0026] Such as Figure 1-4 As shown, the high-precision UAV flight control system includes a charging base station system and a fuselage docking system. The charging base station system includes a matrix landing platform 1, and a plurality of rechargeable grids 2 are installed on the matrix landing platform 1. Each grid A charging power supply 3 is connected to the grid 2; the fuselage docking system includes a plurality of belly contacts 4 installed on the bottom surface of the fuselage and capable of docking with the grid 2.
[0027] In the present invention, the staff is required to establish a matrix landing platform 1 connected to the charging power supply 3 at an appropriate position in advance, and install a plurality of belly contacts 4 that can be docked with the grid 2 on the bottom surface of the fuselage; When there is almost no power, the staff can remotely control the UAV to land on the matrix landing platform 1, dock with the grid 2 through the belly contact 4, ...
Embodiment 2
[0030] Such as Figure 1-4 As shown, the high-precision UAV flight control system includes a charging base station system and a fuselage docking system. The charging base station system includes a matrix landing platform 1, and a plurality of rechargeable grids 2 are installed on the matrix landing platform 1. Each grid A charging power supply 3 is connected to the grid 2; the fuselage docking system includes a plurality of belly contacts 4 installed on the bottom surface of the fuselage and capable of docking with the grid 2.
[0031] In this embodiment, the shape of the grid 2 is square, and the polarity of the electrodes in each grid 2 is the same, so that each side length of the grid 2 can be equal, which helps the belly contact 4 to be connected to the grid 2. butt.
[0032] Preferably, the distance between two adjacent fuselage contacts 4 is greater than the length of the diagonal of a single grid 2, which can ensure that the two fuselage contacts 4 will not land in the...
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