• Title/Summary/Keyword: 스마트다기능시현기

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How to Integrate SMFD Display Software based on Heterogenous Graphic Design Tools (이종 그래픽 저작 도구 기반의 SMFD 화면 시현 소프트웨어 통합 방안)

  • Kyusik Kim;Yongjin Kwon;Seong Han Lee
    • Journal of Aerospace System Engineering
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    • v.18 no.2
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    • pp.79-86
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    • 2024
  • We have developed software for the SMFD that utilizes a range of graphic design tools. These tools enable us to effortlessly create graphic elements by defining their attributes, such as position and motion. Subsequently, we can convert these designs into source code and execute the resulting software on the target system, leveraging the graphic engines provided by the tools. However, when it comes to developing the displaying software for the SMFD using multiple graphic design tools on a single system, we face various challenges. In this paper, we will delve into these challenges and propose solutions for developing the displaying software for SMFD based on heterogeneous display design tools.

A Study on Reliability, Safety Analysis and Related Performance Improvement of Avionics Equipment (항공전자장비 신뢰성, 안전성 분석 및 관련 성능 개선 방안 연구)

  • Seo, Joon-Ho
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.22 no.9
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    • pp.1220-1227
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    • 2018
  • Avionics electronic equipment refers to the electronic equipment installed on an aircraft. Failure of avionics equipment can have a significant impact on aircraft operations as well as threaten the safety of pilots and passengers. Therefore, avionics electronic equipment is required to have higher reliability and safety than electronic equipment used for other purposes. Avionics equipment must consider various component selection and system design to meet reliability and safety-related requirements from the initial design stage. In this paper, we describe safety, reliability performance analysis method of avionics equipment, and introduce various design improvement methods that can be performed to meet safety requirement performance. Finally, the safety performance of the improved avionics equipment was reanalyzed and compared with the value before the improvement, the validity of the proposed design change was verified.