• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.45 no.5
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• pp.417-428
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• 2017

In this paper, we describe the architectural design, unit component hardware design and core software design(Helmet Pose Tracking Software and Terrain Elevation Data Correction Software) of IHDS(Intelligent Helmet Display System), and describe the results of unit test and integration test. According to the trend of the latest helmet display system, the specifications which includes 3D map display, FLIR(Forward Looking Infra-Red) display, hybrid helmet pose tracking, visor reflection type of binocular optical system, NVC(Night Vision Camera) display, lightweight composite helmet shell were applied to the design. Especially, we proposed unique design concepts such as the automatic correction of altitude error of 3D map data, high precision image registration, multi-color lighting optical system, transmissive image emitting surface using diffraction optical element, tracking camera minimizing latency time of helmet pose estimation and air pockets for helmet fixation on head. After completing the prototype of all system components, unit tests and system integration tests were performed to verify the functions and performance.

• Proceedings of the KIEE Conference
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• 2007.07a
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• pp.1868-1869
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• 2007

항공기의 임무컴퓨터는 외부영상과 비행관련 정보들을 시현하기 위한 그래픽 처리를 담당한다. VIOM은 외부영상신호를 임무컴퓨터의 각 모듈에 전달하고, 내부모듈에서 생성한 비행관련정보들을 원하는 시현장치로 전송하는 역할을 한다. 현재 개발하고자 하는 KHP용 임무컴퓨터의 VIOM은 영상수신처리회로, 영상분배 및 선택회로, 모듈영상수신 및 분배회로, 모듈영상선택회로, 그리고 영상선택 정보를 획득하기 위한 데이터 인터페이스 등으로 구성된다. 본 논문은 KHP 임무컴퓨터 VIOM 의 전체 인터페이스 구성과 이를 위한 각 회로 설계에 대한 정보를 제시함을 목적으로 한다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.42 no.4
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• pp.344-350
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• 2014

Multi Function Display(MFD) of Korean Utility Helicopter(KUH) is the component of mission management/display control system and displays image information(navigation, flight, survivability, digital map, maintenance) acquired from Mission Computer(MC) while the aircraft is operated. It is an essential equipment for pilots to perform flight mission and it has functions of display scene control, data display, built in test(BIT) and brightness control. In this paper, it is analyzed the cause of abnormal display(flickering) on MFD and summarized the design changes to solve the defect. It is also described system safety analysis and suggested verification results of flight/ground test.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.46 no.9
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• pp.782-789
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• 2018

Multi-Function Display (MFD) of Korean Utility Helicopter (KUH) displays image information(navigation, flight, topographical and maintenance information) delivered from Mission Computer (MC) during flight operation. The abnormal display of MFD such as flickering phenomenon was identified in the system development. It was solved by improving the shielding performance of the DVI cable and changing the DVI cable installation path at the first mass production. However, it was occurred again when the aircraft was operated for one or two years after delivery. It was also identified in the evaluation process of the derivative helicopters. Therefore, a comprehensive review of the aircraft system level has been performed to solve the problem of MFD malfunction at first and then a design improvement plan was derived by improving the DVI cable. In this paper, the causes of MFD anomalies are analyzed and also the process of design improvement are summarized. The validity of the improvement has been verified through the DVI cable assembly comparison test, SIL/ground/flight test.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.39 no.7
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• pp.660-665
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• 2011

Reconfigurable Flight Simulator for an airborne tactical mission based on virtual reality technology is developed as a software configurable cockpit with computer display as virtual instruments. It can simulate F-15K, KF-16, T/A-50 class fighter and depending on simulated cockpit, control stick and throttle are replaceable. For effective immersion, Video See-Through type HMD is applied.

• Proceedings of the Korea Information Processing Society Conference
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• 2000.04a
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• pp.858-863
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• 2000

동영상은 시간 및 공간적으로 많은 상관성을 지니고 있으며, 움직임추정 방법에서 움직임의 시 공간 상관성을 이용하면 정확한 움직임 추정과 성능 개선을 가져올 수 있다. 한편, Zafar와 Zhang은 웨이브릿 변환 영역에서 가변 블록 (variable block-size)을 이용한 다해상도 움직임 추정(multire-solution motion estimation) 기법을 제안하였다

• Journal of the Korea Institute of Military Science and Technology
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• v.5 no.2
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• pp.72-82
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• 2002

This paper presents the design technology of a Graphic Generator which drives the embedded aircraft display equipments such as HUD(Head-Up Display) and MFD (Multi-Function Display) those provide pilot with the most important mission information. The main issue of this design is how we can implement the real-time embedded graphic generator using a general purpose processor as a substitute for the obsolete the production of specific graphic processor in the military market. So we proposed two kinds of method that one is a software solution so called graphic kernel system, interpreting the display file, controlling the graphic system and pre-processing graphic primitives, the other is a hardware solution so called graphic engine, interpreting passed commands through the graphic kernel system, post-processing the looping calculation taking much of time as implemented by software. We have tested and verified the functionalities and the required performance of Graphic Generator.

• Proceedings of the Korea Information Processing Society Conference
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• 2010.11a
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• pp.789-792
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• 2010

최근 다양하게 활용되고 있는 수치지도 기반의 지도 영상은 그 신속성과 정확성이 가장 중요시되고 있다. 특히, 공군에서 사용하고 있는 지도영상 자료 활용 시스템인 비행 임무 계획 시스템의 상황도 시현 시, 대용량 래스터 데이터(Raster Data)를 처리해야 하는데, 지도의 종류가 다양해지고, 정밀해질수록 시스템의 효율적인 구동에 한계가 발생되고 있는 현실이며, 처리하는 영상의 호환성 및 왜곡현상의 문제점도 함께 야기되고 있다. 이에 본 연구에서는 ARC System 및 RPF Naming Rule을 적용하여 대용량 래스터 데이터 처리과정을 개선하고, 호환성을 보장하며, 왜곡현상을 줄이는 효율적인 지도 영상 처리방안을 제안한다.

• Journal of the Korea Institute of Military Science and Technology
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• v.20 no.5
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• pp.681-687
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• 2017

This paper presents about an implementation of Video Transmitting and Receiving System(VTRS) for acquiring test data. The VTRS consists of two parts. The first is Transmitter Unit(TU) that is installed on a missile to acquire various kinds of data and transmit the data to the ground through RF signals. The second is Receiver Unit(RU) that receives the transmitted RF signals and reconstruct those to the original data. To gather a high speed data reliably and securely on the ground, the TU is designed by considering data transfer scheme, data compression, modulation method, encryption technic, link budget, and antenna radiation pattern. Further, a placement method of multiple receiving stations is suggested. The VTRS has been tested on a field to check the link margins and maximum receiving distance in a real environment. Finally, the VTRS is applied to a missile flight test and gathered high speed data reliably.

• Proceedings of the Korean Society of Computer Information Conference
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• 2011.01a
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• pp.217-220
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• 2011

영상 압축 기술의 발전과 인터넷의 보급으로 사람들은 언제 어디서나 고화질의 미디어를 쉽게 접할 수 있게 되었다. 또한 미디어 플레이어에서 문자열의 출력을 지원함으로써 사용자들은 쉽게 영상의 자막을 만들고 볼 수 있는 환경이 만들어졌다. 그러나 문자는 번역을 위한 역할만 할 뿐 미디어에서 나타내고자 하는 감성을 전달하는 역할은 하지 못한다. 본 연구에서는 애니메이션 캐릭터와 콘텐츠 로봇을 사용하는 새로운 의미전달 기술을 적용한 감성형 콘텐츠 서비스를 제안한다. 제안하는 기술은 동기화 시나리오를 구성하여 미디어가 재생되는 동안 애니메이션 캐릭터 데이터를 제공하며, 또 다른 출력장치인 로봇과 동기화되어 상황에 따른 로봇의 움직임을 통해 시청자에게 내용 전달의 효과와 함께 감성 전달의 효율을 증대시켜주는 역할을 한다. 본 논문에서는 감성형 콘텐츠를 제작한 후 시현을 통해 감성 전달의 효율이 높아짐을 확인하였다.