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WO2012148232A2 - Aircraft instrument display system and method thereof - Google Patents

Aircraft instrument display system and method thereof Download PDF

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Publication number
WO2012148232A2
WO2012148232A2 PCT/KR2012/003322 KR2012003322W WO2012148232A2 WO 2012148232 A2 WO2012148232 A2 WO 2012148232A2 KR 2012003322 W KR2012003322 W KR 2012003322W WO 2012148232 A2 WO2012148232 A2 WO 2012148232A2
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WO
WIPO (PCT)
Prior art keywords
instrument
pilot
template
aircraft
image
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PCT/KR2012/003322
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French (fr)
Korean (ko)
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WO2012148232A3 (en
Inventor
김기일
현세웅
이충재
Original Assignee
경상대학교 산학협력단
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Publication of WO2012148232A2 publication Critical patent/WO2012148232A2/en
Publication of WO2012148232A3 publication Critical patent/WO2012148232A3/en

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00Arrangements or adaptations of instruments
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00Aircraft indicators or protectors not otherwise provided for
    • B64D45/0015Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems
    • B64D45/0051Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems by monitoring passengers or crew on aircraft
    • B64D45/0053Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems by monitoring passengers or crew on aircraft using visual equipment, e.g. cameras
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00Aircraft indicators or protectors not otherwise provided for
    • B64D45/0015Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems
    • B64D45/0051Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems by monitoring passengers or crew on aircraft
    • B64D45/0056Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems by monitoring passengers or crew on aircraft detecting passenger or crew behavior by sensors, e.g. biometrics
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C23/00Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06VIMAGE OR VIDEO RECOGNITION OR UNDERSTANDING
    • G06V10/00Arrangements for image or video recognition or understanding
    • G06V10/10Image acquisition

Definitions

  • the present invention relates to an aircraft instrument display system and a method for displaying and learning a pilot's preferred instrument array after the automatic recognition of identity of the pilot's face image, and more particularly.
  • the left-handed pilot has a problem in that he / she may experience a disruption in response to an instantaneous emergency situation while looking at the instrument panel fixedly arranged for the right-handed.
  • the fixed instrument panel had a problem that it takes time to cope with an emergency because it takes time to check the instrument required by the pilot.
  • the present invention has been made to solve the problems of the prior art as described above, the object of the present invention, in particular, aircraft instrument display system and method for automatically authenticating the pilot to learn and load the preferred instrument arrangement of the pilot To provide.
  • the aircraft instrument display system recognizes a pilot's face image, extracts features of the image, generates a template, and receives the template to check the identity of the pilot, A controller for learning a pilot's preferred instrument arrangement and displaying the instrument's preferred instrument arrangement.
  • the imaging device may include an imaging unit for photographing a pilot's face, a detection unit for receiving the face image and separating the image into respective components, a correction unit for correcting the separated image of the component, and generating a template from the corrected image. And a generating unit for transmitting the generated template.
  • the component includes a face shape, eyes, nose and mouth.
  • the instrument includes an altimeter, speedometer and magnetic world.
  • the learning identifies the frequency and placement position at which the pilot moves, enlarges or reduces the instrument.
  • the control device includes a receiving unit for receiving the template, a comparison unit for extracting a matching template by comparing the template with a plurality of pre-stored templates, a display unit for displaying instrument arrangement information corresponding to the extracted template, and the instrument of the pilot. It includes a learning unit for learning the array to store the preferred instrument array information.
  • the apparatus may further include a storage unit including the plurality of templates and the instrument arrangement information corresponding to the plurality of templates, respectively.
  • the display unit includes a touch pad that recognizes the pilot's touch.
  • an aircraft instrument display method includes an imaging process of photographing a pilot's face, a detection process of receiving the face image and dividing it into respective components, a correction process of correcting an image of the separated component, and correction.
  • a generation process of generating a template from the image, a transmission process of transmitting the generated template, a reception process of receiving the template, a process of extracting a matching template by comparing the template with a plurality of pre-stored templates, and the extracted process A display process of displaying instrument arrangement information corresponding to a template, and a learning process of storing the instrument arrangement information of the pilot by learning the instrument arrangement of the pilot.
  • the pilot is automatically recognized and authenticated, thereby improving the security of the aircraft.
  • FIG. 1 is an exemplary view for showing an aircraft instrument display system according to an embodiment of the present invention as an example.
  • Figure 2 is an exemplary view for showing in detail the imaging device 110 of the aircraft instrument display system 100 of Figure 1 according to an embodiment of the present invention.
  • FIG 3 is an exemplary view for showing in detail the control device 120 of the aircraft instrument display system 100 of Figure 1 according to an embodiment of the present invention.
  • FIG. 4 is an exemplary screen illustrating an example of a meter pattern according to an embodiment of the present invention.
  • FIG. 5 is a flow chart showing an aircraft instrument display method according to an embodiment of the present invention.
  • the basic principle of the present invention is to identify the identity of the pilot's face image to learn the instrument arrangement preferred by the pilot to display the instrument automatically.
  • FIG. 1 is an exemplary view for showing an aircraft instrument display system according to an embodiment of the present invention as an example.
  • the aircraft instrument display system 100 recognizes a face image of a pilot, extracts features of the image, and generates a template, and the template. Receiving a confirmation of the identity of the pilot, learning the preferred instrument arrangement of the pilot, and includes a control device 120 for displaying the instrument arrangement preferred by the pilot.
  • the imaging apparatus 110 separates the recognized pilot's face image for each component, and generates a template by correcting the separated image.
  • the components of the facial image here include the pilot's face shape, eyes, nose and mouth.
  • the imaging device 110 transmits the generated template.
  • control device 120 receives the template and compares it with a plurality of pre-stored templates to select the template that most matches.
  • the plurality of previously stored templates are information stored after generating a template by dividing the face images of the pilots by components.
  • the plurality of pre-stored templates include unique instrument array information learned and stored for each pilot.
  • control device 120 displays the instrument arrangement information according to the selected template.
  • the pilot can then zoom in and out or relocate the displayed instrument array to the instrument of their choice.
  • the relocated gauge array is updated with the gauge array information of the selected template.
  • the display is preferably configured to include a touch pad that can recognize the pilot's touch.
  • the imaging device 110 and the control device 120 according to an embodiment of the present invention will be described in detail with reference to FIGS. 2 to 3.
  • FIG. 2 is an exemplary view for showing in detail the imaging device 110 of the aircraft instrument display system 100 of FIG. 1 according to an embodiment of the present invention.
  • the imaging apparatus 110 includes an imaging unit 111 for imaging a pilot's face, a detection unit 112 for receiving a face image, and separating the components into respective components.
  • a correction unit 113 for correcting an image of the component a generator 114 for generating a template from the corrected image, and a transmitter 115 for transmitting the generated template.
  • the operation of the imaging device 110 according to an embodiment of the present invention configured as shown in FIG. 2 will be described in detail as follows.
  • the imaging unit 111 is configured to include a lens for imaging the pilot's face.
  • the imaging part 111 is a camera. Then, the detector 112 receives the face image picked up by the imaging unit 111 and separates the components into respective components.
  • the components of the facial image include facial contours, eyes, nose, and mouth constituting a human face.
  • the detector 112 separates the transmitted facial image into a facial contour, an eye, a nose, and a mouth.
  • the correction unit 113 then corrects the components separated into facial contours, eyes, noses, and mouths.
  • the eye image when correcting an image of a separated eye, can be positioned in the center of the screen, and the information area can be corrected in binary style by dividing the area with information as '1' and the area without information as '0'. have.
  • the image separated and corrected into the facial contour, eyes, nose, and mouth as described above is generated as a template by the generation unit 114.
  • the transmitter 115 transmits the generated template. That is, the imaging device 110 takes a pilot image and separates it for each component, and then corrects and generates and transmits a template to be compared later.
  • FIG. 3 is an exemplary view for showing in detail the control device 120 of the aircraft instrument display system 100 of FIG. 1 according to an embodiment of the present invention.
  • the control device 120 compares the received template with the template 121 transmitted from the transmitter 115 of FIG. 2, and compares the received template with a plurality of previously stored templates.
  • control device 120 Referring to the operation of the control device 120 according to an embodiment of the present invention configured as shown in Figure 3 in detail as follows.
  • the receiver 121 captures a face image of a specific pilot in the imaging device 110, separates it for each component, and then receives a generated template.
  • the comparison unit 122 compares the received template with a plurality of templates previously stored in the storage unit 125 and extracts the most similar template.
  • the aircraft manager may set a threshold of the degree of correspondence between the templates.
  • the pilot is not authorized to control the instrument information is not loaded and can not control the aircraft.
  • the comparison unit 122 confirms the identity of the pilot, if there is a matching template in the storage unit 125, and transmits the instrument arrangement information of the pilot corresponding to the matching template.
  • the display unit 123 receives and displays instrument arrangement information.
  • the template of pilots stored in the storage unit 125 includes preferred instrument arrangement information for each pilot.
  • the instrument array information is displayed.
  • the pilot can then view the device array information and set the preferred array without further action.
  • the touch screen provided in the display unit 123 may be touched to enlarge and reduce the device and move the position.
  • the learning unit 124 learns the instrument arrangement information of the pilot.
  • the instrument array that the pilot set up can be memorized and loaded on the next flight, and the instrument can load the instrument on the next flight by calculating the arithmetic mean of the frequency of the scaled-up and shifted instruments.
  • FIG. 4 is an exemplary screen illustrating an example of an instrument pattern according to an embodiment of the present invention.
  • the gauge 12 in the gauge 1 of the aircraft may be moved on the screen.
  • gauge 1 and gauge 12 may be repositioned from each other by the touch of a pilot.
  • gauge 2 may be enlarged like gauge 6, and gauge 10 may be reduced like gauge 7.
  • the pilot can reposition the instruments to their tastes and resize each instrument.
  • the instrument placed by the pilot is stored after determining that the frequent arrangement is the pilot's preferred arrangement, and when the pilot is later certified for flight, the instrument array arranged by the pilot is loaded. .
  • the pilot can then artificially store his or her favorite instrument array and load the instrument array that he has saved from the next flight.
  • FIG. 5 is a flowchart showing an aircraft instrument display method according to an embodiment of the present invention.
  • an aircraft instrument display method 500 includes an imaging process of photographing a pilot's face (S510), and a detection process of receiving the photographed face image and separating the components into respective components ( S520), a correction process of correcting the image of the separated component (S530), a generation process of generating a template from the corrected image (S540), a transmission process of transmitting the generated template (S550); Receiving process of receiving a template (S560); Comparing the received templates with a plurality of pre-stored templates and extracting a matching template (S570); A display process 580 for displaying the instrument arrangement information corresponding to the extracted template, and a learning process S590 for learning the instrument arrangement of the pilot and storing the preferred instrument arrangement information.
  • the pilot's face is imaged (S510).
  • each component comprises a facial contour, eyes, nose, mouth and the like that make up the facial image.
  • the image of the separated components is corrected (S530).
  • the eye image is positioned at the center of the screen, and then, the area with the image information is generalized as '1', and the area without the information is generalized as '0'.
  • the template is generated from the corrected image (S540).
  • the generated template is transmitted (S550) and received (S560).
  • the received template is compared with a plurality of pre-stored templates to extract a matching template (S570).
  • the instrument array information corresponding to the extracted template is displayed.
  • the display means for displaying the instrument arrangement information includes a touch screen that can recognize the touch of the pilot.
  • the instrument arrangement thus displayed can be enlarged, reduced and repositioned by the touch of the pilot.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Multimedia (AREA)
  • Theoretical Computer Science (AREA)
  • Image Analysis (AREA)
  • Image Processing (AREA)

Abstract

The present invention relates to an aircraft, and more specifically, to an aircraft instrument display system which automatically recognizes the facial image of a pilot to verify the identity of the pilot, and then displays and memorizes the instrument arrangement preferred by the pilot, and a method thereof. To this end, the present invention comprises: a photographing device which recognizes the facial image of a pilot and extracts the characteristics of the image to generate a template; and a control device which receives the template to verify the identity of the pilot, and memorizes and displays the instrument arrangement preferred by the pilot.

Description

항공기 계기표시 시스템 및 그 방법Aircraft instrument display system and method
본 발명은 항공기에 관한 것으로서 더욱 상세하게는 조종사의 안면 이미지를 자동으로 인식하여 신분을 인증한 후, 조종사의 선호 계기 배열을 디스플레이하고 학습하는 항공기 계기표시 시스템 및 그 방법에 관한 것이다.The present invention relates to an aircraft instrument display system and a method for displaying and learning a pilot's preferred instrument array after the automatic recognition of identity of the pilot's face image, and more particularly.
최근 들어, 항공산업이 활발하게 성장하고 있다. 이에 따라 항공기 조종사들도 그 수가 증가하고 있는 중이다. 그러나 종래에는 항공기를 조종하는 경우, 계기판이 고정되어 있어서 조종사들 마다 고정된 계기판에 적응해야 한다는 불편함이 있었다. 이러한 불편은 항공기와 같이 초고속으로 운행하는 기기에 있어서, 순간적인 실수를 유발하는 경우 대형사고로 이어지는 원인이 되었다.In recent years, the aviation industry has been actively growing. As a result, the number of aircraft pilots is increasing. However, conventionally, when manipulating an aircraft, the instrument panel is fixed, and there is inconvenience that each pilot must adapt to the fixed instrument panel. Such inconvenience caused a large accident in case of causing a momentary mistake in a device that operates at a high speed such as an aircraft.
즉, 왼손잡이의 조종사의 경우 오른손잡이 위주로 고정 배치된 계기판을 보면서 순간적인 비상상황이 발생할 경우 대응에 차질을 겪을 수 있다는 문제점이 상주한다.In other words, the left-handed pilot has a problem in that he / she may experience a disruption in response to an instantaneous emergency situation while looking at the instrument panel fixedly arranged for the right-handed.
한편, 인증되지 않은 조종사가 항공기를 조종할 경우를 대비하여 조종사를 인증하는 경우 그 절차가 복잡하다는 문제점이 있었다.On the other hand, there is a problem that the procedure is complicated in the case of authenticating the pilot in case the uncertified pilot controls the aircraft.
또한, 고정된 계기판은 조종사가 필요한 계기의 확인에도 시간이 걸려 비상사태에 대처하는데 시간이 소요된다는 문제점도 있었다. In addition, the fixed instrument panel had a problem that it takes time to cope with an emergency because it takes time to check the instrument required by the pilot.
따라서, 항공기와 같은 초고속 이동수단에 있어서 비상상황에 신속하게 대처하고 조종사의 피로도를 감소시킬 수 있는 수단이 절실히 요구되고 있다.Therefore, there is an urgent need for a means for rapidly coping with emergency situations and reducing pilot fatigue in ultrafast vehicles such as aircraft.
본 발명은 상술한 바와 같은 종래기술의 문제점을 해결하기 위해 안출된 것으로서, 본 발명의 목적은, 특히 조종사를 자동으로 인증하여 해당 조종사의 선호 계기 배열을 학습하고 로딩시키기 위한 항공기 계기표시 시스템 및 방법을 제공하는 것이다. The present invention has been made to solve the problems of the prior art as described above, the object of the present invention, in particular, aircraft instrument display system and method for automatically authenticating the pilot to learn and load the preferred instrument arrangement of the pilot To provide.
이를 위해 본 발명에 따르는 항공기 계기표시 시스템은, 조종사의 안면 이미지를 인식하고, 상기 이미지의 특징을 추출하여, 템플릿을 생성하는 촬상장치, 및 상기 템플릿을 수신받아 상기 조종사의 신분을 확인하여, 상기 조종사의 선호 계기 배열을 학습하고, 상기 조종사가 선호하는 계기 배열을 디스플레이하는 제어장치를 포함한다.To this end, the aircraft instrument display system according to the present invention recognizes a pilot's face image, extracts features of the image, generates a template, and receives the template to check the identity of the pilot, A controller for learning a pilot's preferred instrument arrangement and displaying the instrument's preferred instrument arrangement.
상기 촬상장치는 조종사의 안면을 촬상하는 촬상부, 상기 안면 이미지를 수신받아 각각의 구성요소로 분리하는 검출부, 분리된 상기 구성요소의 영상을 보정하는 보정부, 보정된 상기 영상으로 템플릿을 생성하는 생성부, 및 생성된 상기 템플릿을 송신하는 송신부를 포함한다.The imaging device may include an imaging unit for photographing a pilot's face, a detection unit for receiving the face image and separating the image into respective components, a correction unit for correcting the separated image of the component, and generating a template from the corrected image. And a generating unit for transmitting the generated template.
상기 구성요소는 얼굴형, 눈, 코, 입을 포함한다.The component includes a face shape, eyes, nose and mouth.
상기 계기는 고도계, 속도계, 자세계를 포함한다.The instrument includes an altimeter, speedometer and magnetic world.
상기 학습은 상기 조종사가 계기를 이동하거나, 확대 또는 축소하는 빈도수와 배치위치를 확인한다.The learning identifies the frequency and placement position at which the pilot moves, enlarges or reduces the instrument.
상기 제어장치는 상기 템플릿을 수신받는 수신부, 상기 템플릿과 기 저장된 복수의 템플릿을 비교하여 일치하는 템플릿을 추출 비교부, 추출된 상기 템플릿에 대응하는 계기 배열 정보를 표시하는 표시부, 및 상기 조종사의 계기 배열을 학습하여 선호하는 계기 배열 정보를 저장시키는 학습부를 포함한다.The control device includes a receiving unit for receiving the template, a comparison unit for extracting a matching template by comparing the template with a plurality of pre-stored templates, a display unit for displaying instrument arrangement information corresponding to the extracted template, and the instrument of the pilot. It includes a learning unit for learning the array to store the preferred instrument array information.
상기 복수의 템플릿과 상기 복수의 템플릿에 각각 대응하는 상기 계기 배열 정보가 포함되어 저장된 저장부를 더 포함한다.The apparatus may further include a storage unit including the plurality of templates and the instrument arrangement information corresponding to the plurality of templates, respectively.
상기 표시부는 상기 조종사의 터치를 인식하는 터치패드를 포함한다. The display unit includes a touch pad that recognizes the pilot's touch.
이를 위해 본 발명에 따르는 항공기 계기표시 방법은 조종사의 안면을 촬상하는 촬상과정, 상기 안면 이미지를 수신받아 각각의 구성요소로 분리하는 검출과정, 분리된 상기 구성요소의 영상을 보정하는 보정과정, 보정된 상기 영상으로 템플릿을 생성하는 생성과정, 생성된 상기 템플릿을 송신하는 송신과정, 상기 템플릿을 수신받는 수신과정, 상기 템플릿과 기 저장된 복수의 템플릿을 비교하여 일치하는 템플릿을 추출과정, 추출된 상기 템플릿에 대응하는 계기 배열 정보를 표시하는 표시과정, 및 상기 조종사의 계기 배열을 학습하여 선호하는 계기 배열 정보를 저장시키는 학습과정을 포함한다.To this end, an aircraft instrument display method according to the present invention includes an imaging process of photographing a pilot's face, a detection process of receiving the face image and dividing it into respective components, a correction process of correcting an image of the separated component, and correction. A generation process of generating a template from the image, a transmission process of transmitting the generated template, a reception process of receiving the template, a process of extracting a matching template by comparing the template with a plurality of pre-stored templates, and the extracted process A display process of displaying instrument arrangement information corresponding to a template, and a learning process of storing the instrument arrangement information of the pilot by learning the instrument arrangement of the pilot.
본 발명의 다양한 실시예에 따르면, 자동으로 조종사를 인식하여 인증함으로써 항공기의 보안을 향상시키는 효과가 있다.According to various embodiments of the present disclosure, the pilot is automatically recognized and authenticated, thereby improving the security of the aircraft.
또한, 본 발명의 다양한 실시예에 따르면, 조종사의 선호 계기 배열을 자동으로 학습하고 표시함으로써 조종사의 항공기 조종을 용이하게 하는 효과도 있다.In addition, according to various embodiments of the present invention, there is also an effect of facilitating the pilot's control of the aircraft by automatically learning and displaying the pilot's preferred instrument arrangement.
본 발명의 다양한 실시예에 따르면, 궁극적으로 조종사의 항공기 조종을 용이하게 함으로써 조종사의 피로 및 스트레스를 감소시키고 긴급상황에서도 기민하게 대처할 수 있는 효과가 있다. According to various embodiments of the present invention, by ultimately facilitating the pilot's control of the aircraft, there is an effect that can reduce the fatigue and stress of the pilot and can be agile even in an emergency.
도 1은 본 발명의 일 실시예에 따르는 항공기 계기표시 시스템을 예를 들어 보여주기 위한 예시도.1 is an exemplary view for showing an aircraft instrument display system according to an embodiment of the present invention as an example.
도 2는 본 발명의 일 실시예에 따르는 도 1의 항공기 계기표시 시스템(100)의 촬상장치(110)를 자세하게 보여주기 위한 예시도.Figure 2 is an exemplary view for showing in detail the imaging device 110 of the aircraft instrument display system 100 of Figure 1 according to an embodiment of the present invention.
도 3은 본 발명의 일 실시예에 따르는 도 1의 항공기 계기표시 시스템(100)의 제어장치(120)를 자세하게 보여주기 위한 예시도.Figure 3 is an exemplary view for showing in detail the control device 120 of the aircraft instrument display system 100 of Figure 1 according to an embodiment of the present invention.
도 4는 본 발명의 일 실시예에 따르는 계기 패턴의 예를 보여주는 화면 예시도.4 is an exemplary screen illustrating an example of a meter pattern according to an embodiment of the present invention.
도 5는 본 발명의 일 실시예에 따르는 항공기 계기표시 방법을 보여주는 순서도.5 is a flow chart showing an aircraft instrument display method according to an embodiment of the present invention.
이하에서는 첨부된 도면들을 참조하여 본 발명의 실시 예에 따른 항공기 계기표시 시스템 및 그 방법을 상세히 설명한다.Hereinafter, with reference to the accompanying drawings will be described in detail the aircraft instrument display system and method according to an embodiment of the present invention.
도 1 내지 도 4의 동일 부재에 대해서는 동일한 도면 번호를 기재하였다.The same reference numerals are used for the same members in FIGS. 1 to 4.
본 발명의 기본 원리는 조종사의 안면 이미지로 신분을 확인하여 조종사가 선호하는 계기배치를 학습하여 자동으로 계기를 디스플레이하는 것이다.The basic principle of the present invention is to identify the identity of the pilot's face image to learn the instrument arrangement preferred by the pilot to display the instrument automatically.
아울러, 본 발명을 설명함에 있어서, 관련된 공지 기능 혹은 구성에 대한 구체적인 설명이 본 발명의 요지를 불필요하게 흐릴 수 있다고 판단된 경우 그 상세한 설명은 생략한다.In addition, in describing the present invention, when it is determined that a detailed description of a related known function or configuration may unnecessarily obscure the subject matter of the present invention, the detailed description thereof will be omitted.
도 1은 본 발명의 일 실시예에 따르는 항공기 계기표시 시스템을 예를 들어 보여주기 위한 예시도이다.1 is an exemplary view for showing an aircraft instrument display system according to an embodiment of the present invention as an example.
도 1을 참조하면 본 발명의 일 실시예에 따르는 항공기 계기표시 시스템(100)은 조종사의 안면 이미지를 인식하고, 상기 이미지의 특징을 추출하여, 템플릿을 생성하는 촬상장치(110), 및 상기 템플릿을 수신받아 상기 조종사의 신분을 확인하여, 상기 조종사의 선호 계기 배열을 학습하고, 상기 조종사가 선호하는 계기 배열을 디스플레이하는 제어장치(120)를 포함한다.Referring to FIG. 1, the aircraft instrument display system 100 according to an exemplary embodiment of the present disclosure recognizes a face image of a pilot, extracts features of the image, and generates a template, and the template. Receiving a confirmation of the identity of the pilot, learning the preferred instrument arrangement of the pilot, and includes a control device 120 for displaying the instrument arrangement preferred by the pilot.
도 1과 같이 구성된 본 발명의 실시 예에 따르는 항공기 계기표시 시스템을 자세히 설명하면 다음과 같다.Referring to the aircraft instrument display system according to an embodiment of the present invention configured as shown in Figure 1 in detail as follows.
우선 촬상장치(110)는 인식한 조종사의 안면 이미지를 구성요소 별로 분리하고, 분리된 이미지를 보정하여 템플릿을 생성한다.First, the imaging apparatus 110 separates the recognized pilot's face image for each component, and generates a template by correcting the separated image.
여기서 안면 이미지의 구성요소는 조종사의 얼굴형, 눈, 코, 입을 포함한다.The components of the facial image here include the pilot's face shape, eyes, nose and mouth.
그리고 촬상장치(110)는 생성된 템플릿을 전송한다.The imaging device 110 transmits the generated template.
그러면 제어장치(120)는 상기 템플릿을 수신받아 기 저장된 복수의 템플릿과 비교하여 가장 많이 일치하는 템플릿을 선택한다.Then, the control device 120 receives the template and compares it with a plurality of pre-stored templates to select the template that most matches.
여기서 기 저장된 복수의 템플릿은 조종사들의 안면 이미지를 구성요소 별로 분리하여 템플릿을 생성한 후 저장된 정보이다.Here, the plurality of previously stored templates are information stored after generating a template by dividing the face images of the pilots by components.
또한, 기 저장된 복수의 템플릿은 조종사들 마다 학습되어 저장된 고유의 계기 배열 정보를 포함한다.In addition, the plurality of pre-stored templates include unique instrument array information learned and stored for each pilot.
따라서 제어장치(120)는 선택된 템플릿에 따른 계기 배열 정보를 디스플레이한다.Therefore, the control device 120 displays the instrument arrangement information according to the selected template.
그러면 조종사는 디스플레이된 계기 배열을 자신이 선호하는 배열로 계기마다 확대 및 축소를 하거나 재배치할 수도 있다.The pilot can then zoom in and out or relocate the displayed instrument array to the instrument of their choice.
즉, 재배치된 계기 배열은 선택된 템플릿의 계기 배열 정보에 업데이트된다.In other words, the relocated gauge array is updated with the gauge array information of the selected template.
이와 같이 조종사에 의해 재배치된 계기 배열은 학습된다.The instrument arrangements thus rearranged by the pilot are learned.
여기서, 디스플레이는 조종사의 터치를 인식할 수 있는 터치패드를 포함하여 구성되는 것이 바람직하다.Here, the display is preferably configured to include a touch pad that can recognize the pilot's touch.
본 발명의 일 실시예에 따르는 촬상장치(110)와 제어장치(120)는 도 2 내지 도 3에서 자세하게 상술하도록 한다.The imaging device 110 and the control device 120 according to an embodiment of the present invention will be described in detail with reference to FIGS. 2 to 3.
도 2는 본 발명의 일 실시예에 따르는 도 1의 항공기 계기표시 시스템(100)의 촬상장치(110)를 자세하게 보여주기 위한 예시도이다.2 is an exemplary view for showing in detail the imaging device 110 of the aircraft instrument display system 100 of FIG. 1 according to an embodiment of the present invention.
도 2를 참조하면 본 발명의 일 실시예에 따르는 촬상장치(110)는 조종사의 안면을 촬상하는 촬상부(111), 안면 이미지를 수신받아 각각의 구성요소로 분리하는 검출부(112), 분리된 구성요소의 영상을 보정하는 보정부(113), 보정된 영상으로 템플릿을 생성하는 생성부(114), 및 생성된 템플릿을 송신하는 송신부(115)를 포함한다.Referring to FIG. 2, the imaging apparatus 110 according to an exemplary embodiment of the present invention includes an imaging unit 111 for imaging a pilot's face, a detection unit 112 for receiving a face image, and separating the components into respective components. A correction unit 113 for correcting an image of the component, a generator 114 for generating a template from the corrected image, and a transmitter 115 for transmitting the generated template.
도 2와 같이 구성된 본 발명의 일 실시예에 따르는 촬상장치(110)의 동작을 자세하게 설명하면 다음과 같다.The operation of the imaging device 110 according to an embodiment of the present invention configured as shown in FIG. 2 will be described in detail as follows.
우선, 촬상부(111)는 조종사의 안면을 촬상하기 위한 렌즈를 포함하여 구성된다.First, the imaging unit 111 is configured to include a lens for imaging the pilot's face.
즉, 촬상부(111)는 카메라인 것이 바람직하다. 그러면 검출부(112)는 촬상부(111)에서 촬상된 안면 이미지를 전송받아 각각의 구성요소로 분리한다.That is, it is preferable that the imaging part 111 is a camera. Then, the detector 112 receives the face image picked up by the imaging unit 111 and separates the components into respective components.
바람직하게 안면 이미지의 구성요소는 사람의 얼굴을 구성하는 안면윤곽이나 눈, 코, 입을 포함한다.Preferably, the components of the facial image include facial contours, eyes, nose, and mouth constituting a human face.
예를 들면 검출부(112)는 전송된 안면 이미지를 안면윤곽, 눈, 코, 입으로 분리한다. 그러면 보정부(113)는 안면윤곽, 눈, 코, 입으로 분리된 구성요소를 보정한다.For example, the detector 112 separates the transmitted facial image into a facial contour, an eye, a nose, and a mouth. The correction unit 113 then corrects the components separated into facial contours, eyes, noses, and mouths.
예를 들면, 분리된 눈의 이미지를 보정하는 경우, 눈동자 이미지를 화면의 중앙에 위치시키고, 정보가 있는 영역을 '1'로 정보가 없는 영역을 '0'으로 구분하여 이진 스타일로 보정할 수 있다.For example, when correcting an image of a separated eye, the eye image can be positioned in the center of the screen, and the information area can be corrected in binary style by dividing the area with information as '1' and the area without information as '0'. have.
이와 같이 안면윤곽, 눈, 코, 입으로 분리되어 보정된 이미지는 생성부(114)에 의해 템플릿으로 생성된다.The image separated and corrected into the facial contour, eyes, nose, and mouth as described above is generated as a template by the generation unit 114.
송신부(115)는 생성된 템플릿을 전송한다. 즉 촬상장치(110)는 조종사의 이미지를 촬상하여 구성요소 별로 분리한 후, 보정하여 차후 비교될 템플릿을 생성하여 전송하는 역할을 한다.The transmitter 115 transmits the generated template. That is, the imaging device 110 takes a pilot image and separates it for each component, and then corrects and generates and transmits a template to be compared later.
도 3은 본 발명의 일 실시예에 따르는 도 1의 항공기 계기표시 시스템(100)의 제어장치(120)를 자세하게 보여주기 위한 예시도이다.3 is an exemplary view for showing in detail the control device 120 of the aircraft instrument display system 100 of FIG. 1 according to an embodiment of the present invention.
도 3을 참조하면 본 발명의 일 실시예에 따르는 제어장치(120)는 도 2의 송신부(115)에서 전송되는 템플릿을 수신받는 수신부(121), 수신된 템플릿과 기 저장된 복수의 템플릿을 비교하여 일치하는 템플릿을 추출하는 비교부(122), 추출된 템플릿에 대응하는 계기 배열 정보를 표시하는 표시부(123), 및 조종사의 계기 배열을 학습하여 선호하는 계기 배열 정보를 저장시키는 학습부(124)를 포함하고, 복수의 템플릿과 그에 따른 계기 배열 정보가 저장된 저장부(125)를 더 포함하여 구성된다. Referring to FIG. 3, the control device 120 according to an embodiment of the present invention compares the received template with the template 121 transmitted from the transmitter 115 of FIG. 2, and compares the received template with a plurality of previously stored templates. A comparator 122 for extracting a matching template, a display unit 123 for displaying gauge array information corresponding to the extracted template, and a learner 124 for learning a pilot array of pilots and storing preferred gauge array information. It includes, and further comprises a storage unit 125 stores a plurality of templates and the resulting instrument arrangement information.
도 3과 같이 구성된 본 발명의 일 실시예에 따르는 제어장치(120)의 동작을 자세하게 설명하면 다음과 같다.Referring to the operation of the control device 120 according to an embodiment of the present invention configured as shown in Figure 3 in detail as follows.
우선, 수신부(121)는 촬상장치(110)에서 특정 조종사의 안면 이미지를 촬상하여 구성요소 별로 분리된 후 보정되어, 생성된 템플릿을 전송받는다.First, the receiver 121 captures a face image of a specific pilot in the imaging device 110, separates it for each component, and then receives a generated template.
그 후, 비교부(122)는 수신된 템플릿과 저장부(125)에 기 저장된 복수의 템플릿을 비교하여 가장 유사한 템플릿을 추출한다.Thereafter, the comparison unit 122 compares the received template with a plurality of templates previously stored in the storage unit 125 and extracts the most similar template.
이때, 항공기 관리자는 템플릿 간 비교 일치도의 임계를 설정할 수 있다.In this case, the aircraft manager may set a threshold of the degree of correspondence between the templates.
예를 들어, 일치도가 60% 미만인 경우, 조종권한이 없는 조종사로 판단하여 계기정보가 로딩되지 않아 항공기의 조종을 할 수 없다.For example, if the degree of agreement is less than 60%, the pilot is not authorized to control the instrument information is not loaded and can not control the aircraft.
또한, 비교부(122)는 조종사의 신분이 확인되고, 저장부(125)에서 일치하는 템플릿이 존재하면, 일치하는 템플릿에 해당하는 조종사의 계기 배열정보를 전송한다.In addition, the comparison unit 122 confirms the identity of the pilot, if there is a matching template in the storage unit 125, and transmits the instrument arrangement information of the pilot corresponding to the matching template.
표시부(123)는 계기 배열정보를 수신받아 디스플레이한다.The display unit 123 receives and displays instrument arrangement information.
여기서 저장부(125)에 저장된 조종사들의 템플릿에는 각각 조종사들 마다 선호하는 계기 배열 정보를 포함하고 있다.Here, the template of pilots stored in the storage unit 125 includes preferred instrument arrangement information for each pilot.
따라서, 조종자가 인증되는 경우, 해당 계기 배열 정보를 디스플레이하는 것이다.Thus, if the operator is authenticated, the instrument array information is displayed.
그러면, 조종사는 해당 기기배열 정보를 보고 별도의 조치없이 선호하는 배열을 세팅할 수 있다.The pilot can then view the device array information and set the preferred array without further action.
만약 조종사가 기기배열 정보를 변경하고 싶은 경우에도 표시부(123)에 구비된 터치스크린을 터치하여 기기의 확대 및 축소, 위치의 이동을 자유자재로 수행할 수 있다.If the pilot wants to change the device arrangement information, the touch screen provided in the display unit 123 may be touched to enlarge and reduce the device and move the position.
이 경우 학습부(124)는 조종사의 계기 배열 정보를 학습한다.In this case, the learning unit 124 learns the instrument arrangement information of the pilot.
즉 조종사가 최종 설정한 계기 배열을 기억하여 다음 비행 때 로딩할 수 있고, 조종사가 확대 축소한 빈도 수와 위치를 이동한 계기들의 빈도수의 산술평균을 구하여 다음 비행 시 계기를 로딩할 수 있다.In other words, the instrument array that the pilot set up can be memorized and loaded on the next flight, and the instrument can load the instrument on the next flight by calculating the arithmetic mean of the frequency of the scaled-up and shifted instruments.
도 4는 본 발명의 일 실시예에 따르는 계기 패턴의 예를 보여주는 화면 예시도이다.4 is an exemplary screen illustrating an example of an instrument pattern according to an embodiment of the present invention.
도 4를 참조하면, 항공기의 계기 1에서 계기 12는 화면상에서 이동이 가능하다.Referring to FIG. 4, the gauge 12 in the gauge 1 of the aircraft may be moved on the screen.
예를 들면, 계기 1과 계기 12는 조종사의 터치에 의해 서로 위치가 변경될 수 있다. 또한, 계기 2도 계기 6처럼 확대될 수 있고, 계기 10도 계기 7과 같이 축소될 수 있다.For example, gauge 1 and gauge 12 may be repositioned from each other by the touch of a pilot. In addition, gauge 2 may be enlarged like gauge 6, and gauge 10 may be reduced like gauge 7.
즉, 조종사는 계기를 자신의 취향에 맞게 재배치할 수 있으며, 각각의 계기의 크기를 조정할 수 있다. 이와 같이 조종사가 계기를 재배치하고 조정함으로써 조종사가 배치한 계기는 빈도 수가 많은 배치가 조종사의 선호 배치라고 판단하여 저장되고, 차후에 조종사가 비행을 위해 인증이 되면 해당 조종사가 배치한 계기 배열이 로딩된다.That is, the pilot can reposition the instruments to their tastes and resize each instrument. As a result of the pilot's rearrangement and adjustment of the instrument, the instrument placed by the pilot is stored after determining that the frequent arrangement is the pilot's preferred arrangement, and when the pilot is later certified for flight, the instrument array arranged by the pilot is loaded. .
그리고 조종사는 자신이 선호하는 계기 배열을 인위적으로 저장하여, 다음 비행부턴 자신이 저장한 계기 배열을 로딩할 수 있다.The pilot can then artificially store his or her favorite instrument array and load the instrument array that he has saved from the next flight.
도 5는 본 발명의 일 실시예에 따르는 항공기 계기표시 방법을 보여주는 순서도이다.5 is a flowchart showing an aircraft instrument display method according to an embodiment of the present invention.
도 5를 참조하면 본 발명의 일 실시예에 따르는 항공기 계기표시 방법(500)은 조종사의 안면을 촬상하는 촬상과정(S510), 촬상된 안면 이미지를 수신받아 각각의 구성요소로 분리하는 검출과정(S520), 분리된 구성요소의 영상을 보정하는 보정과정(S530), 보정된 영상으로 템플릿을 생성하는 생성과정(S540), 생성된 템플릿을 송신하는 송신과정(S550); 템플릿을 수신받는 수신과정(S560); 수신된 템플릿과 기 저장된 복수의 템플릿을 비교하여 일치하는 템플릿을 추출과정(S570); 추출된 템플릿에 대응하는 계기 배열 정보를 표시하는 표시과정(580), 및 조종사의 계기 배열을 학습하여 선호하는 계기 배열 정보를 저장시키는 학습과정(S590)을 포함한다.Referring to FIG. 5, an aircraft instrument display method 500 according to an embodiment of the present invention includes an imaging process of photographing a pilot's face (S510), and a detection process of receiving the photographed face image and separating the components into respective components ( S520), a correction process of correcting the image of the separated component (S530), a generation process of generating a template from the corrected image (S540), a transmission process of transmitting the generated template (S550); Receiving process of receiving a template (S560); Comparing the received templates with a plurality of pre-stored templates and extracting a matching template (S570); A display process 580 for displaying the instrument arrangement information corresponding to the extracted template, and a learning process S590 for learning the instrument arrangement of the pilot and storing the preferred instrument arrangement information.
도 5와 같이 구성됨 본 발명의 일 실시예에 따르는 항공기 계기표시 방법(500)을 자세하게 설명하면 다음과 같다.5 is described in detail with reference to the aircraft instrument display method 500 according to an embodiment of the present invention.
우선 조종사의 안면을 촬상한다(S510).First, the pilot's face is imaged (S510).
그 후 안면 이미지를 수신받아 각각의 구성요소로 분리한다(S520)After receiving the facial image is separated into each component (S520)
바람직하게 각각의 구성요소는 안면 이미지를 구성하는 얼굴윤곽, 눈, 코, 입 등을 포함한다.Preferably each component comprises a facial contour, eyes, nose, mouth and the like that make up the facial image.
이와 같이 분리된 구성요소의 영상은 보정된다(S530).The image of the separated components is corrected (S530).
여기서 영상의 보정을 예를 들어 설명하면 다음과 같다.Herein, the correction of the image is described as follows.
우선 눈의 이미지를 보정하는 경우, 눈동자 이미지를 화면의 중앙에 위치시킨 후, 이미지 정보가 있는 영역은 '1'로, 정보가 없는 영역은 '0'으로 일반화시킨다.First, in the case of correcting an image of an eye, the eye image is positioned at the center of the screen, and then, the area with the image information is generalized as '1', and the area without the information is generalized as '0'.
즉 눈의 이미지를 이진화시키는 것이다.In other words, it binarizes the image of the eye.
이와 같이 보정된 영상으로 템플릿을 생성한다 (S540).The template is generated from the corrected image (S540).
그 후, 생성된 상기 템플릿을 송신하여(S550), 수신받는다 (S560).Thereafter, the generated template is transmitted (S550) and received (S560).
수신받은 템플릿과 기 저장된 복수의 템플릿을 비교하여 일치하는 템플릿을 추출한다(S570).The received template is compared with a plurality of pre-stored templates to extract a matching template (S570).
그러면 추출된 템플릿에 대응하는 계기 배열 정보를 표시한다(580).In operation 580, the instrument array information corresponding to the extracted template is displayed.
바람직하게 계기 배열 정보가 표시되는 표시수단은 조종사의 터치를 인식할 수 있는 터치스크린을 포함하는 것이 바람직하다.Preferably, the display means for displaying the instrument arrangement information includes a touch screen that can recognize the touch of the pilot.
이와 같이 표시된 계기 배열은 조종사의 터치에 의해 확대 및 축소되고 위치가 변경될 수 있다.The instrument arrangement thus displayed can be enlarged, reduced and repositioned by the touch of the pilot.
그러면 조종사의 계기 배열을 학습하여 선호하는 계기 배열 정보를 저장한다 (S590).Then, the pilot arrangement of the instrument to learn and store the preferred instrument arrangement information (S590).
이상과 같이 본 발명은 비록 한정된 실시 예와 도면에 의해 설명되었으나, 본 발명은 상기의 실시 예에 한정되는 것은 아니며, 본 발명이 속하는 분야에서 통상의 지식을 가진 자라면 이러한 기재로부터 다양한 수정 및 변형이 가능하다.As described above, although the present invention has been described with reference to the limited embodiments and the drawings, the present invention is not limited to the above embodiments, and those skilled in the art to which the present invention pertains various modifications and variations from such descriptions. This is possible.
그러므로 본 발명의 범위는 설명된 실시 예에 국한되어 정해져서는 아니 되며, 후술하는 특허청구범위뿐만 아니라 특허청구범위와 균등한 것들에 의해 정해져야 한다.Therefore, the scope of the present invention should not be limited to the described embodiments, but should be determined not only by the claims below but also by the equivalents of the claims.

Claims (7)

  1. 조종사의 안면 이미지를 인식하고, 상기 안면 이미지의 특징을 추출하여, 템플릿을 생성하는 촬상장치; 및An imaging device for recognizing a face image of a pilot, extracting features of the face image, and generating a template; And
    상기 템플릿을 수신받아 상기 조종사의 신분을 확인하여, 상기 조종사가 선호하는 계기 배열을 디스플레이하는 제어장치;를 포함하는 것을 특징으로 하는 항공기 계기표시 시스템.Receiving the template to confirm the identity of the pilot, the controller for displaying the instrument arrangement preferred by the pilot; aircraft instrument display system comprising a.
  2. 제 1항에 있어서, 상기 촬상장치는The method of claim 1, wherein the imaging device
    조종사의 안면을 촬상하는 촬상부;An imaging unit for imaging the pilot's face;
    상기 안면 이미지를 수신받아 각각의 구성요소로 분리하는 검출부;A detector configured to receive the face image and separate the components into respective components;
    분리된 상기 구성요소의 영상을 보정하는 보정부;A correction unit correcting an image of the separated component;
    보정된 상기 영상으로 템플릿을 생성하는 생성부; 및A generation unit generating a template from the corrected image; And
    생성된 상기 템플릿을 송신하는 송신부;를 포함하는 것을 특징으로 하는 항공기 계기표시 시스템.And a transmitter for transmitting the generated template.
  3. 제 1항에 있어서, 상기 제어장치는The method of claim 1, wherein the control device
    상기 조종사가 변경한 계기 배열 상태의 변경이력에 따라 상기 조종사가 선호하는 계기 배열을 학습하는 것을 특징으로 하는 항공기 계기표시 시스템.The aircraft instrument display system, characterized in that for learning the instrument arrangement preferred by the pilot according to the change history of the instrument arrangement state changed by the pilot.
  4. 제 1항에 있어서, 상기 계기는The method of claim 1, wherein the meter
    터치패드 상에 표시되고, 상기 제어장치는 터치패드 상에서 계기 상기 터치패드 상에서의 계기표시 여부, 위치변경, 형태변경, 색상변경, 각 계기의 사용빈도 중 적어도 하나를 확인하여 최종 계기 배열 상태를 상기 조종사가 선호하는 계기 배열로 결정하는 것을 특징으로 하는 항공기 계기표시 시스템.Displayed on the touch pad, the control unit checks at least one of the display of the instrument on the touch pad, the position change, the shape change, the color change, the frequency of use of each instrument to remind the final instrument arrangement state Aircraft instrument display system, characterized in that the pilot determines the preferred instrument arrangement.
  5. 제 1항에 있어서, 상기 제어장치는The method of claim 1, wherein the control device
    상기 템플릿을 수신받는 수신부;Receiving unit for receiving the template;
    상기 복수의 템플릿과 상기 복수의 템플릿에 각각 대응하는 상기 계기 배열 정보가 포함되어 저장된 저장부;A storage unit including the plurality of templates and the instrument arrangement information corresponding to the plurality of templates, respectively;
    상기 템플릿과 상기 저장부에 저장된 상기 복수의 템플릿을 비교하여 일치하는 템플릿을 추출 비교부;Extracting and comparing a template by comparing the template and the plurality of templates stored in the storage unit;
    추출된 상기 템플릿에 대응하는 계기 배열 정보를 표시하는 표시부; 및 A display unit for displaying instrument arrangement information corresponding to the extracted template; And
    상기 조종사의 계기 배열을 학습하여 선호하는 계기 배열 정보를 저장시키는 학습부;를 포함하는 것을 특징으로 하는 항공기 계기표시 시스템.Learning unit for learning the instrument arrangement of the pilot to store the preferred instrument arrangement information; aircraft instrument display system comprising a.
  6. 제 1항과 제3항 내지 제5항 중 어느 한 항에 있어서, 상기 계기는The instrument of claim 1, wherein the instrument is
    고도계, 속도계, 자세계를 포함하는 것을 특징으로 하는 항공기 계기표시 시스템.An aircraft instrument display system comprising an altimeter, speedometer, and own world.
  7. 조종사의 안면을 촬상하는 촬상과정;An imaging process of imaging the pilot's face;
    상기 안면 이미지를 수신받아 각각의 구성요소로 분리하는 검출과정;A detection process of receiving the face image and separating the components into respective components;
    분리된 상기 구성요소의 영상을 보정하는 보정과정;A correction process of correcting the image of the separated component;
    보정된 상기 영상으로 템플릿을 생성하는 생성과정;Generating a template from the corrected image;
    상기 템플릿과 기 저장된 복수의 템플릿을 비교하여 일치하는 템플릿을 추출하는 추출과정;An extraction process of comparing the template with a plurality of pre-stored templates and extracting a matching template;
    추출된 상기 템플릿에 대응하는 계기 배열 정보를 표시하는 표시과정; 및 A display process of displaying instrument arrangement information corresponding to the extracted template; And
    상기 조종사의 계기 배열을 학습하여 선호하는 계기 배열 정보를 저장시키는 학습과정;을 포함하는 것을 특징으로 하는 항공기 계기표시 방법.Learning process for storing the preferred instrument arrangement information by learning the instrument arrangement of the pilot; aircraft instrument display method comprising a.
PCT/KR2012/003322 2011-04-28 2012-04-27 Aircraft instrument display system and method thereof WO2012148232A2 (en)

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