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公开(公告)号:US12097982B2
公开(公告)日:2024-09-24
申请号:US18000291
申请日:2021-05-27
发明人: Takashi Maeda , Hiroki Sato , Tatsuo Makii
摘要: The present disclosure relates to a landing device capable of allowing an unmanned aerial vehicle to be accommodated in a compact manner. A landing device includes a first leg portion that is swingable with a first end portion on a main body side of an unmanned aerial vehicle as an axis; and a second leg portion that is detachably attached to a second end portion of the first leg portion such that the second leg portion extends in an axial direction of the first leg portion. The present disclosure can be applied to, for example, a drone including a camera at a bottom of a main body.
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公开(公告)号:US12012221B2
公开(公告)日:2024-06-18
申请号:US17077766
申请日:2020-10-22
申请人: Airogistic, L.L.C.
发明人: Jeff Michalski , Michael Foley
IPC分类号: B64C39/02 , B64D45/04 , G05D1/00 , G08G5/00 , G08G5/02 , B64U10/00 , B64U10/13 , B64U70/00 , B64U80/00 , B64U101/00
CPC分类号: B64D45/04 , B64C39/024 , G05D1/0669 , G05D1/0676 , G08G5/0013 , G08G5/0026 , G08G5/0065 , G08G5/0069 , G08G5/025 , B64U10/00 , B64U10/13 , B64U70/00 , B64U80/00 , B64U2101/00 , B64U2201/10
摘要: An unmanned aerial vehicle (UAV), a stand for launching, landing, testing, refueling and recharging a UAV, and methods for testing, landing and launching the UAV are disclosed. Further, embodiments may include transferring a payload onto or off of the UAV, and loading flight planning and diagnostic maintenance information to the UAV.
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公开(公告)号:US12001225B2
公开(公告)日:2024-06-04
申请号:US17423123
申请日:2020-01-15
申请人: NILEWORKS INC.
发明人: Chihiro Wake , Hiroshi Yanagishita
CPC分类号: G05D1/0684 , B64C39/024 , B64D45/04 , G05D1/0055 , B64U70/00
摘要: There is provided a drone system in which a drone and a movable body operate in coordination with each other, the movable body being capable of moving with the drone aboard and allowing the drone to make a takeoff and a landing, the drone system includes a demarcating member that demarcates an operation area and detects an intruder into the operation area, the operation area being an area where at least one of the drone and the movable body performs an operation, the movable body includes a movement control section that stops movement of the movable body based on the detection of the intruder by the demarcating member, and the drone includes a landing position determining section that determines a landing position based on a stop position of the movable body.
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公开(公告)号:US11906274B2
公开(公告)日:2024-02-20
申请号:US17753388
申请日:2020-08-20
申请人: BAE SYSTEMS plc
IPC分类号: F42B12/36 , B64C39/02 , H04K3/00 , B63B22/00 , B63G1/00 , F42B10/56 , F42B15/10 , B63G6/00 , B63G9/00 , B64U70/00 , B64U101/20
CPC分类号: F42B12/365 , B63B22/003 , B63G1/00 , B64C39/024 , F42B10/56 , F42B15/10 , H04K3/62 , H04K3/825 , B63G6/00 , B63G2009/005 , B64U70/00 , B64U2101/20 , H04K2203/22
摘要: According to a first aspect of the present invention, there is provided a reconnaissance and communication assembly, adapted to be launched from a gun barrel into the air. The assembly comprises a carrier (with a cavity) and a payload (within the cavity). The payload is arranged to be controllably expelled from the carrier and once expelled from the carrier, the payload transmits a signal.
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公开(公告)号:US11897630B2
公开(公告)日:2024-02-13
申请号:US17079085
申请日:2020-10-23
CPC分类号: B64F1/12 , B64C39/024 , B64F1/007 , B64U70/97 , B64U10/13 , B64U50/34 , B64U70/00 , B64U2201/10
摘要: Methods, systems, and apparatus for drone landing ground station. A method includes determining that a drone is landing on a ground station, based on determining that the drone is landing on the ground station, determining a magnetic field to generate at a first magnetic component at a first position in the ground station and an opposing magnetic polar at a second magnetic component at a second position in the ground station, and generating the magnetic field at the first magnetic component and the opposing magnetic field at the second magnetic component.
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公开(公告)号:US11887488B2
公开(公告)日:2024-01-30
申请号:US17646383
申请日:2021-12-29
CPC分类号: G08G5/0043 , B64C39/024 , G06Q10/00 , G06Q10/10 , G08G5/0013 , G08G5/0034 , G08G5/0069 , G08G5/0082 , B64U10/13 , B64U70/00 , B64U2201/00
摘要: Dispatch of drones is disclosed. Example drone dispatching methods include transmitting a flight plan for a drone to a flight control platform associated with first operator for piloting the drone. The flight plan is based on a first location associated with a service request. In response to receiving a message from the flight control platform, a first communication session between the flight control platform and a flight control unit of the drone is initiated to permit remote piloting of the drone. A drone observation platform associated with a second operator is selected based on a subject matter qualification associated with the second operator and descriptive information included in the service request. A second communication session between the flight control platform and the drone observation platform is initiated for remote piloting of the drone.
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公开(公告)号:US11834197B2
公开(公告)日:2023-12-05
申请号:US16515428
申请日:2019-07-18
发明人: Canlong Lin , Li Wang , Zhimeng Shang
CPC分类号: B64D45/04 , B64C25/24 , G01C5/005 , G05D1/0676 , B64U70/00
摘要: A method for controlling a landing gear of an unmanned aerial vehicle (UAV) includes detecting whether a relative-to-ground height of the UAV is greater than a height threshold, where the relative-to-ground height is a vertical height of the UAV with respect to an object; and in response to the relative-to-ground height being not greater than the height threshold and the UAV having not lowered the landing gear, adjusting the relative-to-ground height to the height threshold or above, and lowering the landing gear.
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公开(公告)号:US11828836B1
公开(公告)日:2023-11-28
申请号:US16556560
申请日:2019-08-30
CPC分类号: G01S13/505 , B64C39/024 , G01S13/581 , G01S13/89 , B64U70/00
摘要: A system and method for detection and identification of an Unmanned Aircraft Systems (UAS) employs a radar system to detect and identify the UAS based on the rich Doppler spectrum generated by one or more rotors and associated motors onboard the UAS. UAS have a low radar cross sections (RCS), relatively low speed, and possess a unique Doppler signature providing data for the system to discriminate once the system detects the quadcopter UAS. The system and method functions as a traditional radar, yet analyzes the micro-Doppler signature, including the RCS and radial speed, to detect and identify the UAS. Based on the signature analysis, the system and method are able to distinguish one model from other types of UAS.
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公开(公告)号:US11822346B1
公开(公告)日:2023-11-21
申请号:US16294597
申请日:2019-03-06
申请人: Snap Inc.
CPC分类号: G05D1/101 , B64C39/024 , G05D1/0016 , B64U50/19 , B64U70/00 , B64U2201/10 , B64U2201/20
摘要: Detection of a launch event of an autonomous vehicle may consider input from a variety of sensors, including acceleration sensors and touch sensors In some aspects, a method includes receiving a first input from a touch sensor, receiving a second input from an accelerometer, determining whether a launch of the autonomous vehicle is detected based on the first input and the second input, and controlling the autonomous vehicle in response to the determining. In some aspects, when a launch is detected, a motor of the autonomous vehicle may be energized. By detecting a launch event in this manner, improved safety and reliability may be realized. A reduced occurrence of false positive launch events may reduce a risk that the motor of the autonomous vehicle is energized when the vehicle has not actually been launched.
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公开(公告)号:US11814172B2
公开(公告)日:2023-11-14
申请号:US17360814
申请日:2021-06-28
发明人: Marc T. Angelucci
IPC分类号: B64C39/02 , B64C27/08 , B64U10/14 , B64U20/87 , B64U30/297 , B64U10/13 , B64U30/20 , B64U50/19 , B64U70/00
CPC分类号: B64C39/024 , B64C27/08 , B64U10/14 , B64U20/87 , B64U30/297 , B64U10/13 , B64U30/20 , B64U50/19 , B64U70/00 , B64U2201/10
摘要: The present disclosure is directed to unmanned aerial vehicle (UAV) comprising a convertible body operably coupled to at least one sensor, and further configured to rotate at least about a longitudinal axis, thereby providing a full field of regard for the at least one sensor, and a plurality of arms extending laterally from the convertible body, each arm of the plurality of arms having a rotor assembly coupled thereto.
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