Portable multitask rotor individual combat unmanned aerial vehicle
A single-soldier, multi-task technology, applied in the field of unmanned aerial vehicles, can solve problems affecting the flight safety of rotor-wing single-soldier combat unmanned aerial vehicles, bird collisions, unmanned aerial vehicle collisions, etc., to improve safety, prevent damage, reduce The effect of resistance
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Embodiment 1
[0029] refer to Figure 1-6, a portable multi-task rotor single-soldier combat UAV, including a fuselage 1 and a radar, the radar is fixedly installed on the fuselage 1, the radar is electrically connected to a receiving module, the receiving module is electrically connected to a single-chip microcomputer, and the single-chip electromechanical The strike module is connected, and the single-chip electromechanical connection is connected with the launch module. The top of the fuselage 1 is fixedly installed with two drive motors 2 arranged symmetrically. The output shaft of the drive motor 2 is welded with a propeller 3. The top of the fuselage 1 is detachable and fixed. Two protective nets 4 arranged symmetrically are installed, and the two propellers 3 are respectively located in the two protective nets 4, a riser 5 is fixedly installed on the middle position of the top of the fuselage 1, and a drainage plate is fixedly installed on the top of the riser 5 6. The bottom of the ...
Embodiment 2
[0038] refer to Figure 1-6 , a portable multi-tasking rotor single-soldier combat UAV, including a fuselage 1 and a radar, the radar is fixedly mounted on the fuselage 1 by screws, the radar is electrically connected to a receiving module, the receiving module is electrically connected to a single-chip microcomputer, and the single-chip microcomputer The strike module is electrically connected, and the single-chip motor is electrically connected to the launch module. The top of the fuselage 1 is fixed with two symmetrical drive motors 2 by screws, and the output shaft of the drive motor 2 is welded with a propeller 3. The top is detachable and fixed with two protective nets 4 arranged symmetrically by screws, and the two propellers 3 are respectively located in the two protective nets 4, and the middle position of the top of the fuselage 1 is fixed with a vertical plate 5 by screws. The top of 5 is fixed with a drainage plate 6 by screws, and the bottom of the fuselage 1 is f...
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