WO2020063631A1 - Dispositif de commande à distance portatif et ensemble système de vol - Google Patents

Dispositif de commande à distance portatif et ensemble système de vol Download PDF

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Publication number
WO2020063631A1
WO2020063631A1 PCT/CN2019/107716 CN2019107716W WO2020063631A1 WO 2020063631 A1 WO2020063631 A1 WO 2020063631A1 CN 2019107716 W CN2019107716 W CN 2019107716W WO 2020063631 A1 WO2020063631 A1 WO 2020063631A1
Authority
WO
WIPO (PCT)
Prior art keywords
flight system
remote control
control device
handheld remote
flight
Prior art date
Application number
PCT/CN2019/107716
Other languages
English (en)
Chinese (zh)
Inventor
王兆喆
张通
Original Assignee
杭州零零科技有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 杭州零零科技有限公司 filed Critical 杭州零零科技有限公司
Publication of WO2020063631A1 publication Critical patent/WO2020063631A1/fr

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/08—Helicopters with two or more rotors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N7/00—Television systems
    • H04N7/18—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00—UAVs characterised by their flight controls
    • B64U2201/20—Remote controls

Definitions

  • the first magnetic component driving mechanism includes a motor, a guide rail, a movable tray connected to the guide rail, and a screw connected to the motor, and the first magnetic component is fixed to the movable tray,
  • the screw is screwed through the threaded hole of the movable tray, and the motor can drive the screw to rotate, so that the movable tray can move up and down along the guide rail, so that the first magnetic component The movement between the first position and the second position.
  • the processing system 22 of the flight system 12 is used to control the operation of the flight system.
  • the processing system 22 is capable of receiving operation instructions from the communication system 24, interpreting the operation instructions as machine instructions, and controlling the flight system components based on the machine instructions (alone or as a group).
  • the processing system 22 can additionally or alternatively process images recorded by the camera, stream the images to the flight system controller 14 (eg, in real time or near real time) or perform any other suitable function.
  • the processing system 22 may include one or more: a processor 32 (e.g., CPU, GPU, etc.), memory (e.g., flash memory, RAM, etc.), or any other suitable processing component.
  • the image frame preferably defines various aspects of the image sampled by the optical sensor 36 (eg, image size, resolution, pixel size and / or shape, etc.).
  • the optical sensor 36 can optionally include a zoom lens, digital zoom, fisheye lens, filter, or any other suitable active or passive optical adjustment.
  • the application of optical adjustments can be actively controlled by the controller, manually controlled by the user 18 (eg, where the user manually sets the adjustment), controlled by the flight system controller 14, or otherwise controlled.
  • the optical system 26 can include a housing that encloses the rest of the optical system components, where the housing is mounted to the body 20.
  • the optical system 26 can be configured in other ways.
  • flight system 12 If the flight system 12 is magnetically coupled to the handheld remote control device 8 and the current to the electromagnet 82 is terminated, the flight system 12 is released from the handheld remote control device 8. Therefore, take-off and landing operations can be achieved by manually or automatically controlling the current applied to the electromagnet 82 and the control instructions sent to the flight system 12.
  • the permanent magnet 86 is fixed to the movable tray 88.
  • the movable tray 88 is slidably coupled to one or more guide rails 90.
  • the quick capture and release coupling mechanism 74 further includes a bracket 92 and a motor 98, and the bracket 92 forms a housing 92A of the quick capture and release coupling mechanism 74.
  • the motor 98 is mounted on a base 92B of the bracket 92.
  • the motor 98 is capable of driving the screw 94 to rotate.
  • the screw 94 is screwed through a threaded hole 96 in the tray.
  • the motor 98 may be any type of suitable motor, including but not limited to a gear motor or a servo motor.
  • Figures 11 and 12 show that the rapid capture and release coupling mechanism 74 uses a permanent magnet or magnetizable material 86 in a lowered position where the distance between the permanent magnet or magnetizable material 86 and the coupler component 84 is maximized, thereby The magnetic force is weakened, so that the permanent magnet or the magnetizable material 86 and the coupler part 84 cannot be effectively magnetically attracted, thereby releasing the coupler part 84 (that is, the flight system 12 is released).

Abstract

L'invention concerne un dispositif de commande à distance portatif (8) et un ensemble système de vol. Le dispositif de commande à distance portatif (8) comprend : une structure de support (72) ; un mécanisme de couplage à capture et libération rapide (74), le mécanisme de couplage à capture et libération rapide (74) étant disposé sur la structure de support (72), et ayant un premier composant magnétique (82) ; et un dispositif de commande (14), le dispositif de commande (14) étant utilisé pour commander le premier composant magnétique (82) de telle sorte que le premier composant magnétique (82) peut avoir au moins un premier état de travail et un second état de travail ; dans le premier état de travail, le premier composant magnétique (82) génère une attraction magnétique avec le second composant magnétique (84) d'un système de vol (12) ; et, dans le second état de travail, le premier composant magnétique (82) ne génère pas d'attraction magnétique avec le second composant magnétique (84) du système de vol (12). L'ensemble système de vol comprend : un dispositif de commande à distance portatif (8) ; et un système de vol (12), le système de vol (12) comprenant un second composant magnétique (84) apte à générer une attraction magnétique avec un premier composant magnétique (82) du dispositif de commande à distance portatif (8).
PCT/CN2019/107716 2018-09-28 2019-09-25 Dispositif de commande à distance portatif et ensemble système de vol WO2020063631A1 (fr)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US201862738251P 2018-09-28 2018-09-28
US62/738,251 2018-09-28
CN201910897267.8A CN110615095B (zh) 2018-09-28 2019-09-23 手持遥控装置和飞行系统套件
CN201910897267.8 2019-09-23

Publications (1)

Publication Number Publication Date
WO2020063631A1 true WO2020063631A1 (fr) 2020-04-02

Family

ID=68923831

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2019/107716 WO2020063631A1 (fr) 2018-09-28 2019-09-25 Dispositif de commande à distance portatif et ensemble système de vol

Country Status (2)

Country Link
CN (1) CN110615095B (fr)
WO (1) WO2020063631A1 (fr)

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TWI809614B (zh) * 2021-11-02 2023-07-21 大陸商廣州昂寶電子有限公司 無人機控制方法和系統以及用於遙控無人機的遙控器

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CN111268126A (zh) * 2020-01-31 2020-06-12 武汉大学 电力巡线无人机无线充电中继站、充电飞控系统及方法
CN113148216A (zh) * 2021-06-02 2021-07-23 南京联汇智能科技有限公司 一种弹射式无人机
CN113859569A (zh) * 2021-10-25 2021-12-31 成都飞机工业（集团）有限责任公司 一种便携式蜂群无人机系统及其使用方法

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CN2476318Y (zh) * 2001-03-27 2002-02-13 美昌玩具制品厂有限公司 玩具车遥控器及可控车辆
US20180101169A1 (en) * 2012-09-22 2018-04-12 Paul G. Applewhite Unmanned Aerial Vehicle Systems and Methods of Use
CN205498797U (zh) * 2016-03-21 2016-08-24 普宙飞行器科技（深圳）有限公司 停机坪及无人机着陆系统
CN205582253U (zh) * 2016-05-10 2016-09-14 南京乐乐飞电子科技有限公司 多功能无人机遥控器
CN205801541U (zh) * 2016-05-31 2016-12-14 南昌理工学院 小型无人机电磁弹射系统
CN206437233U (zh) * 2016-09-08 2017-08-25 厦门九星天翔航空科技有限公司 一种车载无人机起飞装置
CN106516149A (zh) * 2017-01-03 2017-03-22 上海量明科技发展有限公司 飞行器电磁弹射系统及方法
US20180215482A1 (en) * 2017-01-30 2018-08-02 Hanhui Zhang Rotary wing unmanned aerial vehicle and pneumatic launcher
CN206885335U (zh) * 2017-05-09 2018-01-16 昊翔电能运动科技(昆山)有限公司 一种无人机起落架以及无人机
CN207389580U (zh) * 2017-07-28 2018-05-22 中交遥感载荷（北京）科技有限公司 一种无人机降落跟随装置

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TWI809614B (zh) * 2021-11-02 2023-07-21 大陸商廣州昂寶電子有限公司 無人機控制方法和系統以及用於遙控無人機的遙控器

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CN110615095B (zh) 2021-04-13
CN110615095A (zh) 2019-12-27

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