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公开(公告)号:US20250013248A1
公开(公告)日:2025-01-09
申请号:US18891941
申请日:2024-09-20
Applicant: SZ DJI TECHNOLOGY CO., LTD.
Inventor: Junxun ZHONG , Chenxi PENG , Kai WANG , Weihang CHEN
IPC: G05D1/654 , G05D1/606 , G05D1/617 , G05D1/622 , G05D109/20 , G05D111/67
Abstract: A control method is provided, including: obtaining a current altitude of an aircraft, and determining a preset horizontal deviation threshold corresponding to the current altitude; obtaining a current horizontal deviation, wherein the current horizontal deviation is a horizontal deviation between a landing position and a current position of the aircraft; and determining a landing strategy of the aircraft based at least in part on a comparison between the current horizontal deviation and the preset horizontal deviation threshold.
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公开(公告)号:US20220214241A1
公开(公告)日:2022-07-07
申请号:US17605509
申请日:2018-11-29
Applicant: SZ DJI TECHNOLOGY CO., LTD.
Abstract: An unmanned aerial vehicle (UAV) control method includes obtaining target flight data and current flight data; determining a control state variable based on the target flight data and the current flight data; and calibrating a center of gravity of the UAV based on the control state variable.
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公开(公告)号:US20210291982A1
公开(公告)日:2021-09-23
申请号:US17339827
申请日:2021-06-04
Applicant: SZ DJI TECHNOLOGY CO., LTD.
Inventor: Minzhe TAN , Kai WANG , Canlong LIN
Abstract: A method of controlling movement of a plurality of movable devices includes determining, by a processor, at least one of a first priority level or a first safety zone for a first movable device of the plurality of movable devices. The method also includes determining, by the processor, at least one of a second priority level or a second safety zone for a second movable device of the plurality of movable devices based on information relating to the second movable device. The method further includes generating, by the processor, a collision avoidance measure to avoid collision with the second movable device during movement based on at least one of the first priority level, the first safety zone, the second priority level, or the second safety zone.
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4.
公开(公告)号:US20240152162A1
公开(公告)日:2024-05-09
申请号:US18542543
申请日:2023-12-15
Applicant: SZ DJI TECHNOLOGY CO., LTD.
CPC classification number: G05D1/6546 , B64C27/54 , B64D17/80 , B64D45/04 , G05D1/2244 , G05D1/652 , B64D2045/0085
Abstract: An aircraft system includes an aircraft, which further includes at least one propeller to provide a flight power for the aircraft; a communication interface configured to communicate with a parachute; at least one storage medium, storing at least one set of instructions for controlling the aircraft system; and at least one processor in communication with the at least one memory. when the aircraft system is in operation, the at least processor executes the at least one set of instruction to: obtain a propeller locking instruction of the aircraft, and perform a corresponding operation based on the propeller locking instruction. The corresponding operation include a first operation. The first operation, corresponds to a scenario where the aircraft is in a flight state, includes: in response to the propeller locking instruction, the aircraft controlling the at least one propeller to stop and locking the at least one propeller, and deploying the parachute by the aircraft.
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公开(公告)号:US20240126305A1
公开(公告)日:2024-04-18
申请号:US18534743
申请日:2023-12-11
Applicant: SZ DJI TECHNOLOGY CO., LTD.
Inventor: Xianghua JIA , Kai WANG , Lu WANG
CPC classification number: G05D1/667 , B64U50/13 , G05D1/48 , B64U2101/45
Abstract: The present application relates to a control method of an aerial vehicle. The aerial vehicle may comprise a propulsion structure for providing flight power and a spraying apparatus for spraying a material. The control method may comprise determining current target information of the aerial vehicle during a process of the aerial vehicle performing a spraying task, wherein the current target information indicates wind field strength of a downward pressure wind field generated by the propulsion structure; determining, based on the current target information, a desired relative flight altitude of the aerial vehicle corresponding to the current target information relative to the material being sprayed below the aerial vehicle; and controlling the aerial vehicle to fly toward the desired relative flight altitude.
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6.
公开(公告)号:US20210020057A1
公开(公告)日:2021-01-21
申请号:US17033451
申请日:2020-09-25
Applicant: SZ DJI TECHNOLOGY CO., LTD.
Inventor: Chaobin CHEN , Kai WANG
Abstract: A return flight control method includes obtaining return-flight-evaluation information in a return flight mode, controlling an unmanned aerial vehicle (UAV) to return to an alternate landing area in response to that the return-flight-evaluation information satisfies a preset requirement, and controlling the UAV to return to a return point in response to that the return-flight-evaluation information does not satisfy the preset requirement.
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