Control method and device of aircraft and aircraft
A technology of flight control and control method, which is applied in the field of aircraft, can solve the problems that are difficult and the traditional image shooting personnel do not have highly skilled flight control experience, and achieve the effect of getting rid of physical limitations
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Embodiment 1
[0108] image 3 It is a schematic flowchart of an aircraft control method provided by an embodiment of the present invention. The aircraft control method in the embodiment of the present invention can be implemented by the cooperation of various components in the above-mentioned unmanned aerial vehicle, which is not limited here.
[0109] see image 3 , the aircraft control method includes:
[0110] Step 301, acquire virtual rocker parameters.
[0111] Please refer to Figure 4 , the virtual rocker parameters may include at least one of the following parameters: rocker arm length, boom length, distance between the aircraft and the anchor point, the position of the aircraft, and the position of the anchor point.
[0112] Among them, the rocker arm length is the arm length of the virtual rocker arm, which is the length from the top of the boom to the anchor point. The boom length is the liftable range of the virtual rocker, which corresponds to the flying height range of th...
Embodiment 2
[0158] Figure 6 It is a schematic flowchart of another aircraft control method provided by the embodiment of the present invention. Another aircraft control method in the embodiment of the present invention may be executed by a drone, and the embodiment of the present invention is not limited thereto.
[0159] refer to Figure 6 , the aircraft control method includes:
[0160] Step 601, acquire virtual rocker parameters.
[0161] The virtual rocker parameters may include at least one of the following parameters: rocker arm length, boom length, distance between the aircraft and the anchor point, the position of the aircraft, and the position of the anchor point.
[0162] Among them, the rocker arm length is the arm length of the virtual rocker arm, which is the length from the top of the boom to the anchor point. The boom length is the liftable range of the virtual rocker, which corresponds to the flying height range of the aircraft in the embodiment of the present inventi...
Embodiment 3
[0212] Figure 8 It is a schematic diagram of an aircraft control device provided by an embodiment of the present invention. Wherein, the device may be configured in the above-mentioned aircraft.
[0213] refer to Figure 8 , the aircraft control device includes:
[0214] Obtaining module 801, configured to obtain virtual rocker parameters.
[0215] In an embodiment of the present invention, the virtual rocker parameters include at least one of the following parameters:
[0216] The length of the rocker arm, the length of the boom, the distance between the aircraft and the anchor point, the position of the aircraft, and the position of the anchor point.
[0217] Among them, the rocker arm length is the arm length of the virtual rocker arm, which is the length from the top of the boom to the anchor point. The boom length is the liftable range of the virtual rocker, which corresponds to the flying height range of the aircraft in the embodiment of the present invention.
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