• 한국항공운항학회지
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• 제17권3호
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• pp.70-77
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• 2009

We proposed the method of avionics integrated architecture using high-speed fiber optic bus. Typically, data bus of aircraft consists of electronic and optic data transmission method. Avionics systems are difficult to operate the electronic data transmission method for the high speed data processing, synchronization and interconnection between flight control system and flight management system efficiently. In this paper, it is known to look into the problem of data bus and the advanced trend in avionics systems, and propose the appropriate data bus of the advanced avionics systems.

• 항공우주시스템공학회지
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• 제15권6호
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• pp.50-58
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• 2021

Byteflight is developed based on RS-485 communication (an international standard), and it can be used as a data bus during the operation of an integrated avionics system in the latest aircraft. Therefore, the integrated avionics system can perform an effective and safe flight mission only when the accurate and seamless display of flight information, communication, and accurate functions of navigation are implemented. In this study, cause analysis and failure investigation were performed on screen abnormalities and communication interruptions due to signal interference in the Byteflight data bus of the integrated avionics system during aircraft operation. To improve signal interference between avionics units, the branch point and wiring path of the Byteflight data bus were changed, and the verification result of the improved method was also described.

• 한국콘텐츠학회:학술대회논문집
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• 한국콘텐츠학회 2009년도 춘계 종합학술대회 논문집
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• pp.642-647
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• 2009

본 논문은 항공전자통합구조를 위하여 적합한 광통신 데이터 버스를 제안한다. 항공기용 데이터 버스로는 전기식과 광학식 전송 방식을 사용한다. 최근 항공전자시스템은 각 비행제어분야와 비행관리시스템을 관리하는 서버간의 연동 및 동기화, 고속처리 등 기존 버스 방식으로 확장이 힘들다. 따라서 본 논문에서는 이러한 데이터 버스의 문제점을 알아보고 고속광통신기술을 살펴보며 차세대 항공전자 버스 구조로 적합한 방법을 제안한다.

• 한국항공우주학회지
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• 제44권9호
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• pp.825-832
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• 2016

본 논문에서는 항공전자시스템 통합시험에 사용하기 위한 데이터 버스 분석 장비 개발에 대해 기술하였다. 본 데이터 버스 분석 장비는 다양한 인터페이스를 수용할 수 있도록 대부분의 항공전자시스템에 채택되고 있는 MIL-STD-1553B, CAN(Controller Area Network), Ethernet 인터페이스 카드를 갖추었다. 버스 데이터의 수집과 분석을 동시에 효율적으로 수행하기 위해 수집 엔진과 분석 엔진은 각각의 하드웨어를 가진다. 데이터 분석 효율성을 높이기 위해 Grid, 2D 및 3D 형태의 데이터 전시 기능을 제공한다. 데이터 버스 분석 장비의 검증은 시험 절차서에 입각하여 모듈 단위 테스트 및 모듈 간 통합 테스트를 수행하였다. 실제 시험 환경인 비행체 SIL(System Integration Laboratory) 환경에서 수행된 통합시험 결과를 통해 연동 요구도 검증 및 개발된 장비의 유용성을 확인하였다.

• 한국항공운항학회지
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• 제15권1호
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• pp.61-67
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• 2007

The importance and cost of avionics system in the integration of an aircraft is continuously increasing. And we can expect enlarged software portion in the system integration for the more intelligent, reliable, and automated avionics system. Both military and commercial avionics community have moved toward commercial-off-the-shelf(COTS) equipment and open systems architecture not only to increase affordability but also to reduce acquisition cost, shorten development time and risk. The same concept is applied in developing avionics test system used for the avionics system integration test. In this paper, we present important topics in the development of avionics system including real-time operating system, interconnect data bus, software development methodology, software development process, and system integration test.

• 항공우주시스템공학회지
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• 제1권1호
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• pp.60-66
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• 2007

The importance of software development in the integration of an avionics system is continuously increasing. And we can expect enlarged soft ware portion in the system integration for the more intelligent, reliable, and automated avionics system. For an avionics system software development the selection of a real-time operating system and internal avionics data bus protocol is very important from the viewpoint of the integration with the system hardware. In this paper, we present current trend of an avionics system software development including software development methodology, software development process, and international software process assessment improvement model.

• 한국군사과학기술학회지
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• 제14권4호
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• pp.598-606
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• 2011

The importance of avionics systems has increased to a significant level in modern aircraft development. Modern avionics system is a complex integrated system of state-of-art hardware and software technology. Specifying the avionics system architecture is the most important task throughout the avionics system design process. This paper reviews modern avionics system architectures and proposes an effective avionics architecture suitable for modern attack helicopters.

• 한국군사과학기술학회지
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• 제17권4호
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• pp.436-447
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• 2014

The major elements of avionics system architecture are requirements, Real Time Operating System, message communication, memory, and data format etc. Herein describes a state-of-the-art development trend for the avionics system architecture, system requirements and data bus among the major elements of avionics system. While, domestic technology has been tried to Integrated Modular Avionics(IMA) system based on the Avionics Full Duplex Switched Ethernet(AFDX) technology during Light Attack Helicopter(LAH) project in Korea, but not yet proved as the product case in Full Scale Development Phase. The avionics system architecture considering the domestic inexperience of the IMA system architecture are suggested for the Next-generation Corps Unmanned Aircraft System.

• 항공우주기술
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• 제12권2호
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• pp.131-139
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• 2013

본 논문은 소프트 CPU 기반의 소형 전장품 설계 및 개발에 대한 것을 다루고 있다. 소프트 CPU는 소프트웨어를 이용한 로직 합성을 통해서 FPGA 내부에 구성되는 마이크로 프로세서이다. 소형 전장품 개발을 위해 소프트 CPU중 Nios-II 프로세서를 적용하여 다양하고, 다시 구성할구 있고, 다시 조립 가능한 하부 모듈로 설계하고 개발하였다. 모듈 구조로 구성하기 위해서 메인 보드와 하부 보드 모두 전원과 데이터 버스가 공통으로 사용할 수 있도록 구성하였고, 선택적으로 사용할 수 있도록 하였다.

• 한국군사과학기술학회지
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• 제5권2호
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• pp.123-131
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• 2002

ASC(Avionics System Computer) was developed to control weapon delivery and navigation sensors, and to perform man-machine interface with pilots for XKO-1 aircraft. The data communications between ASC and UFC(Up Front Controller), DC(Data Concentrator) were implemented by RS422 serial data bus. Also, SCIL(Standard Computer Interface Library) was designed to facilitate control and management of the computer hardware resources and is embedded in the ASC. These structures have a merit of noise immunity and a reduction of wire harness for signal lines, and enable OFP(Operational Flight Program) programmers to use the SCIL easily without knowing hardware details. Manufactured system was on installed on XKO-1, and peformed for BIT(Built In Test) and interface test with UFC and DC. The test results show that it meets the system requirements.