• Title/Summary/Keyword: 탑재장치

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차량 탑재용 CD 플레이어의 방진 설계

  • 손진승;김규출;오상경
    • Journal of KSNVE
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    • v.7 no.6
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    • pp.894-898
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    • 1997
  • 본 글에서는 차량 탑재형 CD 체인저를 중심으로 차량 탑재형 디스크 플레이어의 방진 설계 절차및 CD 체인저의 방진장치로 가장 적합한 오일 댐퍼의 특성과 그 설계법에 대하여 기술하고자 한다.

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Subsystem simulator using java for the satellite S/W development (위성 S/W 개발을 위한 Java 기반의 Subsystem 시뮬레이터 구축)

  • Shin, Hyun-Kyu;Choi, Jong-Wook;Lee, Jong-In
    • Proceedings of the Korea Information Processing Society Conference
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    • 2008.05a
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    • pp.491-492
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    • 2008
  • 인공위성에 탑재되는 S/W는 위성 내의 다양한 장치들과 유기적으로 통신하며 위성의 동작을 제어하고 임무를 수행한다. 따라서 이들 장치들과의 상호 작용이 충분히 테스트되어야 하나, S/W 개발 과정에서 해당 장치들과 직접 연동되어 개발하기 어려운 경우가 대부분이다. 이에 위성에 탑재되는 다른 장치 및 탑재체의 기능과 역할을 모사할 수 있는 시뮬레이터가 필요성이 대두된다. 본 연구에서는 Java를 이용한 시뮬레이터 개발 방안에 대하여 소개한다.

A Study of the flight s/w test environment for the LEO satellite (저궤도위성 탑재소프트웨어 시험환경에 대한 연구)

  • Chae, Dong-Seok;Lee, Jae-Seung;Choi, Jong-Wook;Yang, Seung-Eun;Lee, Jong-In
    • Aerospace Engineering and Technology
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    • v.6 no.2
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    • pp.45-51
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    • 2007
  • The various levels of test are performed to verify the correctness, completeness, and quality of the developed flight software. The three main test levels are unit test, integration test and verification test. The flight software unit test is performed on the individual PC environment using target simulator. And integration and verification test is mainly performed on STB(S/W Test Bed) which provides test and debugging environments for flight software on the target board This document is to present the test environment for the next generation low earth orbit satellite flight software development.

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Development of Data/Video Transmission System for flying vehicle (비행체 탑재용 데이터/영상 복합전송장치 개발)

  • Cho, Dong-Sik;Ra, Sung-Woong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.11
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    • pp.1052-1057
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    • 2007
  • A highly reliable Video Transmission System (VTS) was developed in order to obtain both video and digital data simultaneously in the real time flight test situation of a flying vehicle. The VTS integrates GPS data, digital telemetry data and video signals into a compact digital data package which is compressed and processed by an MPEG-2 Encoder and a DVB-S modulator respectively. The DVB-S modulator is composed of a specially devised Forward Error Correction processor and base band QPSK modulator. The designed VTS was verified and proved for its required functioning and performance through separate flight tests using an airplane and missiles.

Development of Video Transmission System for Rocket (로켓 탑재를 위한 영상 송수신장치 개발)

  • Cho, Dong-Sik;Rha, Sung-Woong
    • Journal of the Institute of Electronics Engineers of Korea TC
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    • v.46 no.2
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    • pp.60-65
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    • 2009
  • A highly reliable Video Transmission System (VTS) was developed in order to obtain both video and digital data simultaneously in the real time flight test situation of a flying vehicle. The VTS integrates GPS date digital telemetry data and video signals into a compact digital data package which is compressed and processed by an MPEG-2 Encoder and a modulator respectively. The modulator is composed of a specially devised Forward Error Correction processor and base band QPSK modulator. The designed VTS was verified and proved for its required functioning and performance through separate flight tests using an airplane and Rockets.

Design of Air Vehicle Test Equipment for Inspecting On-board Equipment in UAV (무인항공기 탑재장비 점검을 위한 통합 점검 장치 설계)

  • Go, Eun-kyoung;Kwon, Sang-Eun;Song, Yong-Ha
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.25 no.1
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    • pp.108-114
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    • 2021
  • AVTE(Air Vehicle Test Equipment) is a device to check status of on-board aircraft equipment before and after flight for performing successful UAV(Unmanned Aerial Vehicle) missions. This paper describes software design and test sequence of the AVTE for enabling easy-manual check by the operator and convenient automatic check of on-board electric equipment respectively. The proposed AVTE inspects BIT(Built-In Test) results of on-board LRUs(Line Replacement Units) including avionics and sensor sub-system devices. Also, it monitors all the LRU status and check the normality of aircraft equipment by means of setting specific values of the LRUs and confirming the expected test results. The AVTE prints the test results as a form of report to easily check the normal conditions of the aircraft equipment and operates automatically without operator interaction, thus being thought to effectively reduce workload of the operator.

차량 전장용 SW 플랫폼 기술 동향

  • Han, Tae-Man;Seong, Gi-Sun
    • Information and Communications Magazine
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    • v.29 no.2
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    • pp.17-22
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    • 2012
  • 기계식 장치가 주를 이루던 자동차 부품이 최근 전자제어 장치로 크게 변환되면서 차량용 소프트웨어에 대한 연구 개발 및 제품 생산도 크게 늘어나고 있는 추세이다. 자동차의 부품에 소프트웨어가 탑재됨에 따라 공통 모듈의 재 사용성, 부품 호환성 등의 문제점이 생겨나게 되었고 이를 해결하고자 하는 업계 노력의 일환으로 AUTOSAR (AUTomotive Open System Architecture) 표준이 제정된다. 본 고에서는 자동차에 탑재되는 부가 서비스 개발에 있어 기본이 되는 전자장치용 소프트웨어의 표준 플랫폼인 AUTOSAR의 동향 및 이슈에 대해서 알아 본다.

Characteristics of Microwave Propagation for the ETC System (ETC 시스템에서의 마이크로파 전파 특성)

  • 배창호;정희창;김영주;장호성
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.25 no.5A
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    • pp.696-701
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    • 2000
  • Electronic Toll Collection (ETC) System makes the telecommunication possible between the Beacon and the On Board Unit(OBU) for automatic toll collection. In this paper, the propagation path of microwave is modelled and the induced voltage of receiving antenna is analyzed numerically according to multi-path fading effect. In our modelling, we consider frequency, weather condition, polarization and antenna radiation pattern. Also, we suggest the diversity technique in order to reduce the fading effect. In the resuts, the fading effect is reduced significantly in case of the vertical polarization at the rain condition. In general the circular polarization is the most desirable in this application. The antenna which has the high directivity, is also desirable. Using the space and frequency diversity technique at the Beacon, the fading effect is reduced effectively. These results are compared with our experimental data.

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원격탐사위성의 탑재체전송자료 검증을 위한 소프트웨어의 개발

  • Lee, Sang-Taek;Gang, Hyo-Won
    • The Bulletin of The Korean Astronomical Society
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    • v.37 no.2
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    • pp.229.1-229.1
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    • 2012
  • 본 논문에서는 탑재체전송자료 검증을 위한 소프트웨어 개발에 관하여 소개하고자 한다. 원격탐사위성에 탑재되는 고성능원격측정센서는 대용량 데이터를 생성하며 탑재체자료전송장치를 통하여 고주파통신에 의해 지상으로 전송된다. 지상으로 전송되는 대용량 데이터는 다양한 통신경로의 외란으로부터 보호 등을 위하여 채널코딩을 수행된다. 또한 대용량 데이터의 실시간 전송을 위하여 압축이 수행되며 보안을 위한 암호화 역시 수행 된다. 본 논문에서는 이러한 탑재체자료를 검증하기 위한 소프트웨어들과 이러한 소프트웨어의 구성 체계등에 관하여 기술하고 있다.

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Current Development Status of Payload Data Handling Unit for Earth Observation Satellite (지구관측 위성용 탑재체자료처리장치 개발 동향)

  • Lee, Jong-Tae;Lee, Sang-Gyu;Yong, Sang-Soon;Yi, Ho-Sang;Lee, Seung-Kun;Song, Jin-Huan;Kwak, Sin-Ung
    • Current Industrial and Technological Trends in Aerospace
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    • v.9 no.1
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    • pp.90-101
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    • 2011
  • In this article, we introduce the technologies and trend of technical evolution of Payload Data Handling Unit (PDHU) for Earth Observation Satellites. As well, we review the efforts for the Koreanization of PDHU so far, and conclude with some suggestions for future work.

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