Unmanned aerial vehicle flight control system and unmanned aerial vehicle
A flight control system and flight control technology, applied in the field of unmanned aerial vehicles, can solve the problems of non-normal use, poor fault tolerance, and inability to control the command transmission flight control circuit board, etc., so as to improve fault tolerance performance and avoid flight accidents.
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Embodiment 1
[0040] figure 1 It is a schematic structural diagram of the UAV flight control system provided by Embodiment 1 of the present invention. Such as figure 1 As shown, the present embodiment provides a UAV flight control system, including:
[0041] A flight control main board 1, a plurality of flight control sub-boards 2, each flight control sub-board 2 is connected to the flight control main board 1;
[0042] The flight control main board 1 is used to generate a start signal through the enabling module 15 on the flight control main board 1, and send the start signal to the flight control sub-board 2;
[0043] The flight control sub-board 2 is used to receive the start signal sent by the flight control main board 1, and activate the flight control mode after receiving the start signal, and send a control signal to the flight control main board 1;
[0044] The flight control main board 1 is also used to receive the control signals sent by each flight control sub-board 2, and jud...
Embodiment 2
[0064] image 3 It is a schematic structural diagram of the drone provided by Embodiment 2 of the present invention. Such as image 3 As shown, the present embodiment provides a drone, including:
[0065] The drone body 4, and the drone flight control system 5 as described in the first embodiment.
[0066] For the specific implementation scheme of this embodiment, refer to the relevant descriptions in the above-mentioned embodiment of the flight control system for the UAV, which will not be repeated here.
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