Gravity center balancing method of unmanned aerial vehicle and unmanned aerial vehicle
A drone and trim technology, applied in the field of drones, can solve problems such as crashes of drones, difficulty in flying drones normally and smoothly, and affecting normal operation of drones, so as to improve flight reliability and service life , Ensure load consistency, improve service life and reliability
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Embodiment 1
[0041] figure 1 The structure diagram of the unmanned aerial vehicle provided for the embodiment of the present invention, such as figure 1 As shown, this embodiment provides an unmanned aerial vehicle, which can be applied to fields such as border patrol, aerial photography, distribution, construction site surveying and mapping, agricultural plant protection, and manned flight. This embodiment does not discuss specific application scenarios of unmanned aerial vehicles. limit. In this embodiment, the drone is taken as an example of a manned drone for description, but it can be understood that the drone provided by the present invention can also be a non-manned drone.
[0042] Specifically, the UAV includes a body 3, a rotor 2, a flight control system, a center of gravity trimming device 1, a landing gear 4, and the like. The body 3 is made of metal material, which provides support and protection for the whole drone, and the body 3 is arranged symmetrically along its longitud...
Embodiment 2
[0060] This embodiment provides a method for balancing the center of gravity of an unmanned aerial vehicle and an unmanned aerial vehicle. Compared with the first embodiment, the basic structure of the unmanned aerial vehicle provided by this embodiment is the same as that of the first embodiment, only the rotor 2 and the flight controller There are differences in system settings, and this embodiment will not repeat the same structure as that of Embodiment 1.
[0061] In this embodiment, only one set of rotors 2 is provided, and the central axis of rotation of the rotors 2 passes through the center of gravity of the drone itself. The drive control unit includes a steering gear, and there are multiple steering gears for controlling the periodic pitch of the propeller in the rotor 2 so as to adjust the flight attitude of the drone.
[0062] The setting of the single-rotor UAV is a conventional setting in this field, and this embodiment does not limit and repeat the specific stru...
Embodiment 3
[0065] This embodiment provides a drone, and compared with Embodiment 1 and Embodiment 2, there is only a difference in the setting of the center of gravity balance device 1 in this embodiment, other settings of the drone can refer to Embodiment 1 or implement Setting is performed in Example 2, which will not be repeated in this embodiment.
[0066] The center of gravity balance device 1 provided by this embodiment includes: a first rail 11 and a second rail 12 connected vertically, the first rail 11 can rotate around the center line of its length direction, and the second rail 12 can rotate along the center line of the first rail 11. Sliding along the length direction, the counterweight 13 is slidably connected to the second track 12 , and the counterweight 13 can slide along the length direction of the second track 12 .
[0067] The center of gravity balance device 1 provided in this embodiment can make the counterweight 13 slide on the second rail 12, the second rail 12 sli...
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