WO2020230964A1 - Device for displaying flight area on ground and operation method therefor - Google Patents
Device for displaying flight area on ground and operation method therefor Download PDFInfo
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- WO2020230964A1 WO2020230964A1 PCT/KR2019/014048 KR2019014048W WO2020230964A1 WO 2020230964 A1 WO2020230964 A1 WO 2020230964A1 KR 2019014048 W KR2019014048 W KR 2019014048W WO 2020230964 A1 WO2020230964 A1 WO 2020230964A1
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- Prior art keywords
- ground
- flight area
- displaying
- flight
- fall
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- 238000000034 method Methods 0.000 title claims abstract description 17
- 230000001133 acceleration Effects 0.000 claims description 11
- 230000005856 abnormality Effects 0.000 description 6
- 238000010586 diagram Methods 0.000 description 5
- 238000005259 measurement Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 230000007423 decrease Effects 0.000 description 1
- 239000004973 liquid crystal related substance Substances 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000011017 operating method Methods 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
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- G—PHYSICS
- G03—PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
- G03B—APPARATUS OR ARRANGEMENTS FOR TAKING PHOTOGRAPHS OR FOR PROJECTING OR VIEWING THEM; APPARATUS OR ARRANGEMENTS EMPLOYING ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ACCESSORIES THEREFOR
- G03B21/00—Projectors or projection-type viewers; Accessories therefor
- G03B21/14—Details
- G03B21/20—Lamp housings
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- G—PHYSICS
- G03—PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
- G03B—APPARATUS OR ARRANGEMENTS FOR TAKING PHOTOGRAPHS OR FOR PROJECTING OR VIEWING THEM; APPARATUS OR ARRANGEMENTS EMPLOYING ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ACCESSORIES THEREFOR
- G03B21/00—Projectors or projection-type viewers; Accessories therefor
- G03B21/14—Details
- G03B21/20—Lamp housings
- G03B21/2046—Positional adjustment of light sources
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- 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
- B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
Definitions
- an unmanned aerial vehicle As a technology for an unmanned aerial vehicle, in particular, it relates to an unmanned aerial vehicle displaying a flight area on the ground, and an operating method thereof.
- Drones are equipped with various sensors depending on the purpose of navigation, control and use.
- drones are equipped with GPS, geomagnetic sensors, and inertial navigation devices for navigation, and use radar, LiDAR, and cameras to avoid obstacles at close range, surveillance and reconnaissance, and monitoring of specific targets.
- An object of the present invention is to provide an apparatus for displaying a flight area on the ground and a method of operating the same.
- an apparatus for displaying a flight area on the ground includes: a light generating unit that projects an image using a beam; And a control unit for controlling the light generation unit, and the control unit may control the light generation unit to project a predetermined image to a predetermined position on the ground during flight.
- the apparatus for displaying the flight area on the ground may further include a sensor unit for generating sensor information by detecting at least one of altitude, speed, acceleration, and attitude.
- the controller may determine whether to project an image of the light generator based on the sensor information.
- the controller may calculate the fall position or fall angle of the unmanned aerial vehicle based on the sensor information.
- the controller may control the light generator to project a predetermined image based on the calculated fall position or fall angle.
- the light generating unit includes a projector that projects a beam and at least one motor connected to the projector, and the control unit calculates a projection angle to project a predetermined image based on the calculated fall position or fall angle, and controls the motor based on the projection angle. I can.
- the controller may determine at least one of a beam width, a beam intensity, and a focus of the light generator based on the sensor information.
- the method of informing the flight area by a device for displaying a flight area on the ground including a light generating unit for projecting an image using a beam and a control unit for controlling the light generating unit includes altitude, speed, and acceleration of the unmanned flight unit. And generating sensor information by detecting at least one of a posture. And controlling the light generator to project a predetermined image to a predetermined position on the ground during flight based on the sensor information.
- a device that displays the flight area on the ground has an effect of notifying people on the ground that the unmanned flight device is in flight by displaying the flight area on the ground.
- FIG. 1 is a block diagram of an apparatus for displaying a flight area on the ground according to an exemplary embodiment.
- FIG. 2 is an exemplary view illustrating a method of projecting a beam by an apparatus for displaying a flight area on the ground according to an example.
- FIG 3 is an exemplary diagram for explaining a method of projecting a beam by an apparatus for displaying a flight area on the ground according to another example.
- FIG. 4 is a configuration diagram of a light generator according to an embodiment.
- FIG. 5 is a flowchart illustrating a method of projecting a beam by an apparatus for displaying a flight area on the ground according to an exemplary embodiment.
- FIG. 1 is a block diagram of an unmanned aerial vehicle according to an embodiment.
- an apparatus 100 for displaying a flight area on the ground may include a light generating unit 110 and a control unit 120.
- the light generator 110 may project an image using a beam.
- the light generation unit 110 projects a predetermined image such as a CRT (Cathode Ray Tube) projector, an LCD (Liquid Crystal Display) projector, a DLP (Digital Light Processing) projector, a laser projector, a logo light, a laser pointer, etc. It may include at least one of displayable devices.
- the controller 120 may control the light generating unit 110 to project a predetermined image to a predetermined position on the ground during flight.
- the controller 120 may control the light generator 110 by determining whether to project a predetermined image. For example, the controller 120 may determine whether to project a predetermined image according to the altitude of the device 100 that displays the flight area on the ground. For example, the controller 120 may determine to project a predetermined image only when the altitude is higher than or equal to a predetermined altitude, and thus control the light generation unit 110.
- the predetermined image is an image indicating that the device 100 that displays the flight area on the ground in the sky is in flight or the flight area of the device 100 that displays the flight area on the ground. It can be an image.
- a predetermined image may be composed of figures, characters, symbols, and the like.
- the apparatus 100 for displaying a flight area on the ground may further include a sensor unit (not shown) that generates sensor information by sensing at least one of altitude, speed, acceleration, and attitude.
- the sensor unit may include at least one of a global positioning system (GPS) and an inertial measurement device (IMU).
- GPS global positioning system
- IMU inertial measurement device
- the inertial measurement device may sense linear acceleration using one or more accelerometers and sense rotational speed using one or more gyroscopes.
- the controller 120 may determine whether the light generator 110 projects an image based on sensor information.
- the control unit 120 can know the altitude of the unmanned airfield * 100 from the sensor information, and based on the altitude, the light generator 110 can be turned on/off or the beam projection can be turned on/off. have.
- the controller 120 may calculate a fall position of the device 100 that displays a flight area on the ground based on sensor information. For example, when the device 100 for displaying the flight area on the ground is in a stationary state in the air, the control unit 120 displays the flight area on the ground when an abnormality occurs. It can be assumed that the device 100 will fall vertically below.
- the device 100 for displaying the flight area on the ground when the device 100 for displaying the flight area on the ground is flying at a predetermined speed in a predetermined direction at a predetermined altitude, the device 100 for displaying the flight area on the ground when an abnormality occurs It can fall freely in the direction of parabolic motion according to the law of motion. Accordingly, when an abnormality occurs, the controller 120 may estimate that the device 100 for displaying the flight area on the ground will fall to a point distant from the current position by a predetermined distance in a predetermined direction.
- the controller 120 may calculate a fall angle based on sensor information of the device 100 that displays the flight area on the ground. For example, the controller 120 may calculate 0 o as a fall angle based on a vertical direction when falling from a stop state. In addition, the controller 120 may calculate a fall angle in a direction in which the angle increases as the flight speed of the apparatus 100 for displaying the flight area on the ground increases. On the other hand, the controller 120 may calculate a fall angle in a direction in which the angle decreases as the altitude of the apparatus 100 for displaying the flight area on the ground increases. The fall angle according to speed or altitude may be determined according to the law of parabolic motion according to free fall.
- the controller 120 may calculate a fall position or fall angle in real time using sensor information.
- the controller 120 may store information on a fall position or fall angle according to an altitude, speed, acceleration, etc. of the device 100 that displays a flight area on the ground, and the corresponding information according to sensor information Can be read.
- the controller 120 may control the light generating unit 110 to project a predetermined image based on the calculated fall position or fall angle.
- the unmanned flight device 210 including a device for displaying a flight area on the ground may be located in the air in a stationary state.
- the controller 120 may control the light generating unit 110 to project a predetermined image 215 in the vertical downward direction of the unmanned aerial vehicle 210.
- the unmanned aerial vehicle 220 including a device displaying a flight area on the ground may fly at a predetermined speed in a predetermined direction at a predetermined altitude.
- the flight device 220 may fall to a point away from the current position by a predetermined distance in a predetermined direction.
- the controller 120 may calculate the fall position or fall angle of the unmanned aerial vehicle 220 when an abnormality occurs, and based on this, control the light generation unit 110 to project a predetermined image 225 have.
- control unit 120 may determine at least one of a beam width, a beam intensity, and a focus of the light generator 110 based on sensor information.
- a method of controlling the light generating unit 110 by the controller 120 is described on the assumption that the altitude of the unmanned aerial vehicle is increased.
- the unmanned aerial vehicle 310 including a device displaying a flight area on the ground can project a predetermined image 315 on the ground, and at this time, the beam width May be the first beam width 313.
- a predetermined image 325 may be projected with the second beam width 323 as shown in FIG. 3(b).
- a predetermined image area may increase in proportion to the altitude squared.
- the controller 120 may increase the beam intensity by controlling the light generator 110 according to the elevation of the image.
- the controller 120 may control the light generating unit 110 to adjust the focus according to the altitude.
- the controller 120 may reduce the beam width by controlling the light generation unit 110 according to the elevation of the altitude.
- the controller 120 controls the light generator 110 to adjust the beam intensity based on the beam width. I can.
- the control unit 120 may calculate the predicted fall range based on any one of information on the flight status and external status of the unmanned aerial vehicle.
- the controller 120 may determine the beam width based on the predicted fall range, and control the light generator 110 based on this to adjust the beam width.
- FIG. 4 is a configuration diagram of a light generator according to an embodiment.
- the light generation unit 400 may include a projector 410 that projects a beam and one or more motors 420 connected to the projector.
- the unmanned aerial vehicle 220 including a device for displaying a flight area on the ground may fly at a predetermined speed in a predetermined direction at a predetermined altitude, and in this case, the unmanned flight device ( 220) may fall to a point distant from the current position in a predetermined direction. Accordingly, the controller 120 may calculate the fall position or fall angle of the unmanned aerial vehicle 220 when an abnormality occurs, and based on this, control the light generation unit 110 to project a predetermined image 225 have.
- the controller 120 may determine a first angle 231 to project an image by calculating a fall position or a fall angle. Also, the controller 120 may control the projection angle of the projector 410 by controlling the motor 420 based on the first angle 231. However, when the unmanned aerial vehicle 220 moves in a predetermined direction, the posture may be inclined by a predetermined angle. As shown in FIG. 2(b), the unmanned aerial vehicle 220 may fly while inclined by the second angle 233. Accordingly, when the control unit 120 controls the motor 420 based on only the first angle 231 to control the projection angle of the projector 410, the position at which the image is projected may be different.
- control unit 120 may obtain the attitude information of the unmanned aerial vehicle through the sensor unit, through which the second angle 233 may be known. Accordingly, the controller 120 may control the projection angle of the projector 410 by controlling the motor 420 based on the first angle 231 and the second angle 233. Through this, the controller 120 may correct an error in which the position at which the image is projected may vary due to the posture of the unmanned aerial vehicle.
- FIG. 5 is a flowchart illustrating a method of projecting a beam by an apparatus for displaying a flight area on the ground according to an exemplary embodiment.
- a device displaying a flight area on the ground may generate sensor information by detecting at least one of altitude, speed, acceleration, and attitude of the unmanned aerial vehicle (510).
- an apparatus for displaying a flight area on the ground may include a sensor unit that generates sensor information by detecting at least one of altitude, speed, acceleration, and posture.
- the sensor unit may include at least one of a global positioning system (GPS) and an inertial measurement device (IMU).
- GPS global positioning system
- IMU inertial measurement device
- the inertial measurement device may sense linear acceleration using one or more accelerometers and sense rotational speed using one or more gyroscopes.
- the device for displaying the flight area on the ground may control the light generating unit 520 to project a predetermined image to a predetermined position on the ground during flight based on the sensor information.
- the device displaying the flight area on the ground may determine whether to project an image of the light generator based on sensor information.
- the device for displaying the flight area on the ground may calculate the fall position or fall angle of the unmanned aerial vehicle based on sensor information.
- the apparatus for displaying the flight area on the ground may control the light generating unit to project a predetermined image based on the calculated fall position or fall angle.
- One aspect of the present invention may be implemented as a computer-readable code in a computer-readable recording medium. Codes and code segments implementing the above program can be easily inferred by a computer programmer in the art.
- the computer-readable recording medium may include any type of recording device storing data that can be read by a computer system. Examples of computer-readable recording media may include ROM, RAM, CD-ROM, magnetic tape, floppy disk, optical disk, and the like. Further, the computer-readable recording medium can be distributed over a computer system connected by a network, and written and executed in computer-readable code in a distributed manner.
- the apparatus for displaying the above-described flight area on the ground can be applied to various unmanned flight apparatuses.
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- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Traffic Control Systems (AREA)
- Navigation (AREA)
Abstract
Description
Claims (8)
- 비행 영역을 지상에 표시하는 장치에 있어서,In the device for displaying the flight area on the ground,빔을 이용하여 이미지를 투사하는 광 발생부; 및 A light generating unit that projects an image using a beam; And상기 광 발생부를 제어하는 제어부를 포함하며,It includes a control unit for controlling the light generating unit,상기 제어부는 The control unit비행 시 지상의 소정 위치에 소정의 이미지를 투사하도록 상기 광 발생부를 제어하는, 비행 영역을 지상에 표시하는 장치.A device for displaying a flight area on the ground, which controls the light generating unit to project a predetermined image on the ground during flight.
- 제 1 항에 있어서,The method of claim 1,상기 무인 비행 장치는 고도, 속도, 가속도 및 자세 중 적어도 하나를 감지하여 센서 정보를 생성하는 센서부를 더 포함하는, 비행 영역을 지상에 표시하는 장치.The unmanned flight device further comprises a sensor unit for generating sensor information by detecting at least one of altitude, speed, acceleration, and posture, and displaying a flight area on the ground.
- 제 2 항에 있어서, The method of claim 2,상기 제어부는 상기 센서 정보에 기초하여 상기 광 발생부의 이미지 투사 여부를 결정하는, 비행 영역을 지상에 표시하는 장치.The control unit determines whether to project an image of the light generating unit based on the sensor information, and displays a flight area on the ground.
- 제 2 항에 있어서,The method of claim 2,상기 제어부는 상기 센서 정보를 기초로 상기 무인 비행 장치의 추락 위치 또는 추락 각도를 계산하는, 비행 영역을 지상에 표시하는 장치.The controller calculates a fall position or fall angle of the unmanned aerial vehicle based on the sensor information, and displays a flight area on the ground.
- 제 4 항에 있어서,The method of claim 4,상기 제어부는 상기 계산된 추락 위치 또는 추락 각도에 기초하여 상기 소정의 이미지를 투사하도록 상기 광 발생부를 제어하는, 비행 영역을 지상에 표시하는 장치.The control unit controls the light generating unit to project the predetermined image based on the calculated fall position or fall angle, and displays a flight area on the ground.
- 제 4 항에 있어서,The method of claim 4,상기 광 발생부는 빔을 투사하는 프로젝터 및 상기 프로젝터와 연결된 하나 이상의 모터를 포함하며, The light generator includes a projector for projecting a beam and at least one motor connected to the projector,상기 제어부는 The control unit상기 계산된 추락 위치 또는 추락 각도에 기초하여 상기 소정의 이미지를 투사할 투사각을 계산하며,Calculate a projection angle to project the predetermined image based on the calculated fall position or fall angle,상기 투사각에 기초하여 상기 모터를 제어하는, 비행 영역을 지상에 표시하는 장치.A device for displaying a flight area on the ground, which controls the motor based on the projection angle.
- 제 2 항에 있어서,The method of claim 2,상기 제어부는 상기 센서 정보에 기초하여 상기 광 발생부의 빔 폭, 빔 세기 및 초점 중 적어도 하나를 결정하는, 비행 영역을 지상에 표시하는 장치.The control unit determines at least one of a beam width, a beam intensity, and a focus of the light generator based on the sensor information.
- 빔을 이용하여 이미지를 투사하는 광 발생부 및 상기 광 발생부를 제어하는 제어부를 포함하는 비행 영역을 지상에 표시하는 장치가 비행 영역을 알리는 방법에 있어서, In the method for displaying a flight area on the ground, an apparatus for displaying a flight area including a light generating unit for projecting an image using a beam and a control unit for controlling the light generating unit,상기 무인 비행 장치의 고도, 속도, 가속도 및 자세 중 적어도 하나를 감지하여 센서 정보를 생성하는 단계; 및Generating sensor information by detecting at least one of altitude, speed, acceleration, and posture of the unmanned aerial vehicle; And상기 센서 정보에 기초하여 비행 시 지상의 소정 위치에 소정의 이미지를 투사하도록 상기 광 발생부를 제어하는 단계를 포함하는, 무인 비행 장치가 비행 영역을 알리는 방법.And controlling the light generating unit to project a predetermined image to a predetermined position on the ground during flight based on the sensor information.
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KR1020190055604A KR102200182B1 (en) | 2019-05-13 | 2019-05-13 | An unmanned aerial vehicle for displaying flight areas on the ground and its operating method |
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US20120069589A1 (en) * | 2010-09-22 | 2012-03-22 | Willeke Benjamin | Led landing light arrangement for an aircraft |
KR101496892B1 (en) * | 2014-06-19 | 2015-03-03 | 충남대학교산학협력단 | Multicopter dron |
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KR20170086194A (en) * | 2016-01-18 | 2017-07-26 | 김성호 | Fall warning device and uav having the same |
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JP6239567B2 (en) * | 2015-10-16 | 2017-11-29 | 株式会社プロドローン | Information transmission device |
KR101824183B1 (en) * | 2016-08-08 | 2018-02-01 | 드론스페이스 (주) | Drone with drop prevention function |
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US6161798A (en) * | 1998-04-30 | 2000-12-19 | Van Sise, Jr.; Robert B. | Emergency warning device |
US20120069589A1 (en) * | 2010-09-22 | 2012-03-22 | Willeke Benjamin | Led landing light arrangement for an aircraft |
KR101496892B1 (en) * | 2014-06-19 | 2015-03-03 | 충남대학교산학협력단 | Multicopter dron |
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