-
公开(公告)号：US20240174386A1
公开(公告)日：2024-05-30
申请号：US18522455
申请日：2023-11-29
Applicant: AUTEL ROBOTICS CO., LTD.
IPC: B64U20/83
Abstract: The embodiments of the present disclosure disclose an aircraft, including a housing, a first drive module, a first antenna module, a second drive module, a third drive module and a fourth drive module. The first drive module includes a first arm and a first drive assembly, one end of the first arm is arranged on the housing, and the first drive assembly is arranged at the other end of the first arm; the first antenna module is arranged at the other end of the first arm, and the first antenna module is located above the first drive assembly; and the second drive module includes a second arm and a second drive assembly, one end of the second arm is arranged on the housing, and the second drive assembly is arranged at the other end of the second arm.
-
公开(公告)号：US20240166329A1
公开(公告)日：2024-05-23
申请号：US18512340
申请日：2023-11-17
Applicant: AUTEL ROBOTICS CO., LTD.
Inventor： Kangli WANG , Ao HE
Abstract: The present disclosure discloses an unmanned aerial vehicle. The unmanned aerial vehicle includes a wing and a fuselage that are detachably connected to each other, a first protruding portion and a second protruding portion are formed at a position of the fuselage that corresponds to the wing, the first protruding portion and the second protruding portion are arranged opposite to each other, a mounting groove configured to accommodate a middle portion of the wing is formed between the first protruding portion and the second protruding portion, a mounting hole is formed on the first protruding portion and/or the second protruding portion, a pin hole is formed at a position of the middle portion of the wing that corresponds to the mounting hole, an index pin is arranged on the fuselage, the index pin is fixed on the first protruding portion and/or the second protruding portion, the index pin includes a bolt, and the bolt partially runs through the mounting hole and extends into the pin hole. In the present disclosure, the wing and the fuselage can be connected through the index pin. Therefore, the wing and the fuselage may be detachably connected to each other and conveniently detached from each other. In addition, through cooperation among the first protruding portion, the second protruding portion and the wing, flight and aerodynamic performance of the unmanned aerial vehicle can be ensured, and an appearance is aesthetic and concise.
-
93.发明公开公开(公告)号：US20240153122A1
公开(公告)日：2024-05-09
申请号：US18178220
申请日：2023-03-03
Applicant: AUTEL ROBOTICS CO.,LTD.
Inventor： Xin ZHENG
IPC: G06T7/593 , B64U20/70 , G05D1/243 , H04N13/239 , H04N13/282 , H04N23/90
CPC classification number: G06T7/596 , B64U20/70 , G05D1/2435 , H04N13/239 , H04N13/282 , H04N23/90 , G05D2109/254
Abstract: A binocular vision-based environment sensing method and apparatus, is applied to an unmanned aerial vehicle. The unmanned aerial vehicle is provided with five binocular cameras. The first binocular camera is disposed at the front portion of the fuselage of the unmanned aerial vehicle. The second binocular camera is inclined upward and disposed between the left side of the fuselage and the upper portion of the fuselage of the unmanned aerial vehicle. The third binocular camera is inclined upward and disposed between the right side of the fuselage and the upper portion of the fuselage of the unmanned aerial vehicle. The fourth binocular camera is disposed at the lower portion of the fuselage of the unmanned aerial vehicle. The fifth binocular camera disposed at the rear portion of the fuselage of the unmanned aerial vehicle. The method can simplify an omni-directional sensing system while reducing the sensing blind area.
-
94.发明公开公开(公告)号：US20240071234A1
公开(公告)日：2024-02-29
申请号：US18239538
申请日：2023-08-29
Applicant: AUTEL ROBOTICS CO., LTD.
Inventor： Xiaomeng HUANG
IPC: G08G5/00
CPC classification number: G08G5/0039 , G08G5/0013
Abstract: A method and a system for controlling a flight device, a storage medium and an electronic device are provided. The method includes: acquiring a mission flight route of a first flight device, where the mission flight route is configure to indicate a flight route of a data acquisition mission to be performed by the first flight device; generating a relay flight route of the second flight device according to the mission flight route and a relay base station distribution on the mission flight route, where the relay flight route is configured to indicate a flight route of the second flight device during execution of the data acquisition mission by the first flight device; and controlling the first flight device to perform the data acquisition mission according to the mission flight route and controlling the second flight device to perform the data acquisition mission according to the relay flight route.
-
公开(公告)号：US20240058717A1
公开(公告)日：2024-02-22
申请号：US18494335
申请日：2023-10-25
Applicant: AUTEL ROBOTICS CO., LTD.
Inventor： Huihua ZHANG , Zhiying LIANG
CPC classification number: A63H30/04 , G05G9/04796 , G05G9/06 , G08C17/02 , G05G2009/04744 , G05G2009/04777
Abstract: A remote control includes a body, a first rocker device, a second rocker device, a processor, and a signal transmission device. The first rocker device and the second rocker device are installed on the body. The processor connects to the first rocker device, the second rocker device, and the signal transmission device. The first rocker device includes a joystick component. The second rocker device includes a second joystick component. When the first joystick component moves in parallel relative to the body, the processor generates a remote control instruction used to control a movable object to move in a horizontal plane. When the second joystick component moves straightly relative to the body along a first direction or a second direction, the processor generates a remote control instruction used to control the movable object to move upward or move downward in a vertical direction of the movable object.
-
Patent Agency Ranking
公开(公告)号：US20240043146A1
公开(公告)日：2024-02-08
申请号：US18485576
申请日：2023-10-12
Applicant: AUTEL ROBOTICS CO., LTD.
Inventor： Qiang LIU
CPC classification number: B64U30/12 , B64U10/20 , B64C29/0033
Abstract: Embodiments of the present disclosure relate to the technical field of unmanned aerial vehicles, in particular to a tiltable wing and an unmanned aerial vehicle. The tiltable wing includes a wing body, a wingtip, a power device, a cable, a rotating shaft and a driving mechanism. The power device is mounted on the wingtip; one end of the cable is connected to the power device, the rotating shaft is rotatably connected to the wing body and the wingtip, respectively, a through hole is disposed in an axial direction of the rotating shaft, and the other end of the cable passes through the through hole and extends to the inside of the wing body; the driving mechanism is used for driving the wingtip to rotate with the rotating shaft as an axis; and the power device is switchable between a first preset position and a second preset position relative to the wing body, so that the power device is switched between a horizontal state and a vertical state.
-
97.发明授权公开(公告)号：US11889193B2
公开(公告)日：2024-01-30
申请号：US17661322
申请日：2022-04-29
Applicant: AUTEL ROBOTICS CO., LTD.
Inventor： Zhaozao Li
CPC classification number: H04N23/69 , H04N5/2628 , H04N7/183 , H04N23/57 , H04N23/66
Abstract: The embodiments are a zoom method and apparatus, an unmanned aerial vehicle, an unmanned aircraft system and a storage medium. The zoom method is applied to an unmanned aerial vehicle including an image capturing apparatus and the method includes: controlling the image capturing apparatus to capture an initial image, where a resolution of the initial image is W0*H0 and an area of the initial image is S0; obtaining a cropped image according to the initial image, where the cropped image is an image with an area of S cropped from a preset region in the initial image, S0/S=C and C is a digital zoom factor of the image capturing apparatus; and obtaining a zoom image according to the cropped image, where the zoom image is an image obtained by zooming the cropped image by C/A times, a resolution of the zoom image is W1*H1, A=W0/W1 and C≤A.
-
公开(公告)号：US11877253B2
公开(公告)日：2024-01-16
申请号：US17659890
申请日：2022-04-20
Applicant: AUTEL ROBOTICS CO., LTD.
Inventor： Zhaozao Li
CPC classification number: H04W56/0055 , H04J3/0635 , H04W4/40
Abstract: The embodiments are an aircraft time synchronization system and method. The system comprises: a first communication module and a second communication module, wherein data transmission is performed between the first communication module and the second communication module via a communication line, and an I/O interface of the first communication module is connected to the I/O interface of the second communication module via an interruption signal line; the first communication module sends the data information to the second communication module via the communication line, and at the same time sends the triggered interruption signal to the second communication module via the interruption signal line; the second communication module performs time synchronization with the first communication module based on the communication time difference and system time difference with the first communication module determined according to the receiving time of the data information and interruption signal and the sending time.
-
公开(公告)号：US20240010368A1
公开(公告)日：2024-01-11
申请号：US18219080
申请日：2023-07-06
Applicant: AUTEL ROBOTICS CO., LTD.
Inventor： Jianlong LIAO , Yuelong LIAO
Abstract: An unmanned aerial vehicle (UAV) assembly includes an UAV and an UAV docking station. The UAV docking station includes a housing, an extension piece, and a door. The housing is provided with an accommodation cavity and a hatch communicating with the accommodation cavity. The extension piece comprises an extension cavity and is connected to the housing. The extension piece is disposed on a side portion of a housing end which is near the hatch, and the extension cavity communicates with the accommodation cavity. The door is connected to the housing and disposed at the hatch, and the door is configured to open or close the hatch. A cross-sectional area where the extension cavity communicates with the accommodation cavity is greater than a cross-sectional area of the accommodation cavity. The UAV can be accommodated in the accommodation cavity of the UAV docking station.
-
公开(公告)号：US20240004051A1
公开(公告)日：2024-01-04
申请号：US18215654
申请日：2023-06-28
Applicant: Autel Robotics Co., Ltd.
Inventor： Feng TAO , Yanfeng Dang
IPC: G01S13/34 , G01S7/35 , G01S13/536 , G05D1/10
CPC classification number: G01S13/347 , G01S7/356 , G01S13/536 , G05D1/106
Abstract: A radar ranging method and a ranging radar are applied to an unmanned aerial vehicle. A first range to an obstacle is obtained using a first radar waveform. range. A second range to the obstacle are obtained using a second radar waveform if the first range is less than a preset switching threshold. the maximum detection range of the first radar waveform is greater than that of the second radar waveform; and a detection range resolution of the second radar waveform is higher than that of the first radar waveform.
-
-
-
-
-
-
-
-
-
Search Results
414
records
(took 0.028 seconds)
