Electric multi-rotor aircraft and control method
A multi-rotor aircraft and rotor technology, applied in the field of flight, can solve the problems of difficult control of manned aircraft and easy occurrence of safety accidents, etc.
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no. 1 example
[0027] Please refer to figure 1 , figure 1 It is a schematic structural diagram of an electric manned flight system 100 provided in a preferred embodiment of the present invention. The electric manned flight system 100 includes an electric multi-rotor aircraft 10 and a manned device 20 . The electric multi-rotor aircraft 10 is connected with the manned device 20 .
[0028] Please refer to figure 2 , figure 2 show figure 1 The structural schematic diagram of the electric multi-rotor aircraft 10 shown in . The electric multi-rotor aircraft 10 includes a frame assembly 11 , a lift assembly 12 and a plurality of motor rotors 13 . The lift component 12 and a plurality of motor rotors 13 are respectively fixed on the frame component 11 , and the motor rotors 13 are symmetrically distributed around the lift component 12 .
[0029]The frame assembly 11 includes a central frame 111 , a first boom 112 , a second boom 113 , a third boom 114 and a fourth boom 115 . The first can...
no. 2 example
[0041] Please refer to Figure 5 , Figure 5 It is a flowchart of steps of a control method provided by a preferred embodiment of the present invention. The method is applied to an electric multi-rotor aircraft 10 provided in the first embodiment. Such as Figure 5 As shown, the method may include the following steps:
[0042] In step S101, the controller 30 obtains corresponding control instructions in response to user operations.
[0043] In this embodiment, the control instructions include a first instruction, a second instruction, a third instruction and a fourth instruction.
[0044] Step S102 , the controller 30 detects the tilt direction information of the electric multi-rotor aircraft 10 through the gyroscope 50 .
[0045] In this embodiment, the tilt direction information includes first tilt direction information, second tilt direction information, third tilt direction information, and fourth tilt direction information.
[0046] Step S103, when the controller 30...
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