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WO2017219200A1 - Véhicule aérien sans pilote - Google Patents

Véhicule aérien sans pilote Download PDF

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Publication number
WO2017219200A1
WO2017219200A1 PCT/CN2016/086398 CN2016086398W WO2017219200A1 WO 2017219200 A1 WO2017219200 A1 WO 2017219200A1 CN 2016086398 W CN2016086398 W CN 2016086398W WO 2017219200 A1 WO2017219200 A1 WO 2017219200A1
Authority
WO
WIPO (PCT)
Prior art keywords
unmanned aerial
aerial vehicle
uav
target
photographing device
Prior art date
Legal status (The legal status 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 status listed.)
Ceased
Application number
PCT/CN2016/086398
Other languages
English (en)
Chinese (zh)
Inventor
李珂悦
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to PCT/CN2016/086398 priority Critical patent/WO2017219200A1/fr
Publication of WO2017219200A1 publication Critical patent/WO2017219200A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/02—Gyroplanes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00—Constructional aspects of UAVs
    • B64U20/80—Arrangement of on-board electronics, e.g. avionics systems or wiring
    • B64U20/87—Mounting of imaging devices, e.g. mounting of gimbals
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/13—Flying platforms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/30—Supply or distribution of electrical power
    • B64U50/31—Supply or distribution of electrical power generated by photovoltaics

Definitions

  • the invention relates to the field of unmanned aerial vehicle detection technology, and in particular to an unmanned aerial vehicle.
  • An unmanned aerial vehicle is an unmanned aerial vehicle that is operated by a radio remote control device or its own program control device.
  • Unmanned aerial vehicles are divided into large unmanned aerial vehicles and small unmanned aerial vehicles. According to their functions, they can be divided into military and civilian.
  • the flying hand manually controls the unmanned aerial vehicle, which is not only inefficient, the captured image is blurred and not coherent, and the manual operation is easy to cause a safety hazard.
  • the propeller of the existing unmanned aerial vehicle generates a large noise during the flight, and the noise generated by the propeller itself may affect the shooting effect.
  • the main object of the invention is to provide an unmanned aerial vehicle, which aims to solve the technical defects that the existing unmanned aerial vehicle cannot track the target for shooting and the noise affects the shooting effect.
  • the invention provides an unmanned aerial vehicle comprising an unmanned aerial vehicle main body, a plurality of rotors, a telescopic rod and a photographing device, wherein the unmanned aerial vehicle main body is connected to the rotor and the telescopic rod,
  • the telescopic rod is disposed under the UAV main body, and the photographing device is disposed at an end of the telescopic rod, wherein: the rotor provides flight power to the UAV to make the UAV Flying in the air;
  • the UAV host controls the telescopic rod to extend a preset distance to move the photographing device away from the rotor preset distance;
  • the UAV host is configured to control the photographing according to an initial target image
  • the device tracks the live image of the target in the air.
  • the invention can track the target in real time, and shoot the target in real time, improve the shooting efficiency of the unmanned aerial vehicle, avoid the manual control of the unmanned aerial vehicle tracking target by the flying hand, and reduce the flying hand control.
  • the difficulty of the aircraft improves the safety factor of the unmanned aerial vehicle.
  • the photographing device is away from the propeller preset distance to avoid the propeller rotation of the unmanned aerial vehicle The noise generated during the transition affects the shooting effect.
  • Figure 1 is a schematic view showing the structure of a preferred embodiment of the invention unmanned aerial vehicle
  • Figure 2 is a schematic view of a preferred embodiment of the invention in which the telescopic rod is elongated in an unmanned aerial vehicle;
  • FIG. 3 is a schematic diagram showing the internal structure of a preferred embodiment of an unmanned aerial vehicle host in the invention of an unmanned aerial vehicle.
  • Fig. 1 is a schematic structural view of a preferred embodiment of the invention unmanned aerial vehicle.
  • the unmanned aerial vehicle 100 includes, but is not limited to, an unmanned aerial vehicle main body 1, a plurality of rotors 2 (for example, four rotors), a plurality of tripods 3 (for example, two tripods), Telescopic rod 4 and imaging device 5.
  • the UAV main engine 1 is connected to the rotor 2, the stand 3 and the telescopic rod 4. Specifically, the stand 3 and the telescopic rod 4 are disposed below the UAV main unit 1.
  • the imaging device 5 is disposed at an end of the telescopic rod 4.
  • the rotor 2 provides flight power to the unmanned aerial vehicle 100.
  • the stand 3 is used to provide support for the UAV 100 to dock on the ground.
  • the telescopic rod 4 can be telescoped to adjust the relative position between the camera 5 and the rotor 2 (as shown in FIG. 2). Specifically, the UAV host 1 controls the telescopic rod 4 to extend a predetermined distance so that the photographing device 5 is away from the rotor 2 by a predetermined distance (for example, 20 meters or 30 meters).
  • Each rotor 2 includes a support arm 20, a motor 22, and a propeller 24 that is driven by a motor 22.
  • One end of the support arm 20 is connected to the UAV main body 1 , the other end of the support arm 20 is fixed to the motor 22 , and the propeller 24 is disposed above the motor 22 .
  • the photographing device 5 is used for tracking a live image of a photographing target in the air.
  • the target refers to a human body or a specific object (for example, a car, a soccer field, etc.).
  • the camera device 5 is a 360 degree panoramic camera or a 360 degree rotating camera.
  • the UAV host 1 is configured to control the photographing device 5 to track a real-time image of the target in the air according to the initial target image.
  • the telescopic rod 4 is extended downward before the photographing device 5 is operated.
  • the preset distance to reduce the noise of the propeller 24 has an adverse effect on the shooting.
  • the unmanned aerial vehicle 100 is a small unmanned aerial vehicle operated by a radio remote control device or a self-program control device, such as an unmanned fixed-wing aircraft, an unmanned multi-rotor aircraft, a small unmanned aerial vehicle such as an unmanned wing aircraft. .
  • the battery 6 can be mounted inside or outside the UAV main unit 1. In other embodiments, the battery 6 may also be disposed on the support arm 20 on which the rotor 2 is disposed.
  • the battery may be, but not limited to, a solar cell, a rechargeable battery (eg, a lithium ion battery), or the like.
  • Fig. 3 is a schematic view showing the internal structure of a preferred embodiment of the unmanned aerial vehicle main unit 1 of the invention unmanned aerial vehicle.
  • the UAV host 1 includes, but is not limited to, a target setting unit 202, a flight control unit 203, and a communication unit 204.
  • the UAV host 1 is also connected to the imaging device 5 and the battery 6.
  • the target setting unit 202 is configured to set an initial target image. Specifically, the target setting unit 202 controls the photographing device 4 to take an initial image taken by an aiming target (for example, a human body or a specific object), which is an initial target image, before starting aerial photography.
  • an aiming target for example, a human body or a specific object
  • the flight control unit 203 controls the UAV 100 to track the target in real time in the air according to the initial target image and to perform real-time shooting of the target by the photographing device 4.
  • the communication unit 204 is a wireless communication interface with remote wireless communication function, for example, a communication interface supporting communication technologies such as GSM, GPRS, CDMA, WiMAX, FDD-LTE, TD-LTE, and the display with the remote end.
  • the terminal (not shown) performs wireless communication.
  • the communication unit 204 transmits the real-time image of the target to the remote display terminal, and displays the display terminal Show.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Remote Sensing (AREA)
  • Studio Devices (AREA)

Abstract

L'invention concerne un véhicule aérien sans pilote (100) comprenant une unité principale (1) de véhicule aérien sans pilote, de multiples rotors (2), une tige télescopique (4) et un dispositif de photographie (5). L'unité principale (1) de véhicule aérien sans pilote est reliée aux rotors (2) et à la tige télescopique (4). La tige télescopique (4) est disposée au-dessous de l'unité principale (1) de véhicule aérien sans pilote. Le dispositif de photographie (5) est disposé à l'extrémité distale de la tige télescopique (4). Les rotors (2) fournissent au véhicule aérien sans pilote (100) la puissance nécessaire pour voler de façon à permettre au véhicule aérien sans pilote (100) d'être aéroporté. L'unité principale (1) de véhicule aérien sans pilote commande la tige télescopique (4) pour l'étendre jusqu'à une distance prédéterminée de façon à éloigner le dispositif de photographie (5) des rotors (2) de la distance prédéterminée. L'unité principale (1) de véhicule aérien sans pilote est utilisée pour commander, en se basant sur une image cible initiale, le dispositif de photographie (5) en vue de suivre de manière aérienne une cible et de photographier des images en temps réel de celle-ci. Le véhicule aérien sans pilote (100) est capable de suivre la cible en temps réel et de photographier la cible en temps réel, augmentant ainsi l'efficacité de photographie du véhicule aérien sans pilote (100) et empêchant que les effets de photographie soient affectés par le bruit produit par les rotors (24) du véhicule aérien sans pilote (100) lors de la rotation.
PCT/CN2016/086398 2016-06-20 2016-06-20 Véhicule aérien sans pilote Ceased WO2017219200A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/CN2016/086398 WO2017219200A1 (fr) 2016-06-20 2016-06-20 Véhicule aérien sans pilote

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/CN2016/086398 WO2017219200A1 (fr) 2016-06-20 2016-06-20 Véhicule aérien sans pilote

Publications (1)

Publication Number Publication Date
WO2017219200A1 true WO2017219200A1 (fr) 2017-12-28

Family

ID=60783692

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2016/086398 Ceased WO2017219200A1 (fr) 2016-06-20 2016-06-20 Véhicule aérien sans pilote

Country Status (1)

Country Link
WO (1) WO2017219200A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112867395A (zh) * 2018-10-30 2021-05-28 株式会社尼罗沃克 行驶路径生成系统、行驶路径生成方法和行驶路径生成程序以及无人机

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101236994B1 (ko) * 2012-10-31 2013-02-26 네이버시스템(주) 항공사진 촬영용 카메라의 초점위치 안정화 지지대
CN204433078U (zh) * 2015-01-30 2015-07-01 深圳市大疆创新科技有限公司 云台及使用该云台的飞行器
CN104859857A (zh) * 2015-06-02 2015-08-26 宋南 一种单镜头全景无人机系统
CN204660022U (zh) * 2015-04-07 2015-09-23 徐鸿博 一种八旋翼飞行器
CN204776013U (zh) * 2015-06-04 2015-11-18 东莞中寰智能航空科技有限公司 一种六轴无人机

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101236994B1 (ko) * 2012-10-31 2013-02-26 네이버시스템(주) 항공사진 촬영용 카메라의 초점위치 안정화 지지대
CN204433078U (zh) * 2015-01-30 2015-07-01 深圳市大疆创新科技有限公司 云台及使用该云台的飞行器
CN204660022U (zh) * 2015-04-07 2015-09-23 徐鸿博 一种八旋翼飞行器
CN104859857A (zh) * 2015-06-02 2015-08-26 宋南 一种单镜头全景无人机系统
CN204776013U (zh) * 2015-06-04 2015-11-18 东莞中寰智能航空科技有限公司 一种六轴无人机

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112867395A (zh) * 2018-10-30 2021-05-28 株式会社尼罗沃克 行驶路径生成系统、行驶路径生成方法和行驶路径生成程序以及无人机

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