• Title/Summary/Keyword: Avionics System

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Analysis of KASS Flight Test Requirements using The EGNOS (EGNOS 사례를 활용한 KASS 비행시험 요구 사항 분석)

  • Son, Sung-Jin;Hong, Gyo-young;Hong, Woon Ki;Kim, Koon-Tack
    • Journal of Advanced Navigation Technology
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    • v.21 no.6
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    • pp.579-584
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    • 2017
  • SBAS is a satellite based navigation correction system that provides correction information and integrity information of GNSS signal through geostationary satellite based on analysis of GNSS signal in ground station. KASS, a Korean SBAS, is aiming at the APV-1 class SoL service in 2022. Sufficient ground and flight tests must be performed in advance to provide SoL services. However, since KASS, the Korean SBAS, has not yet been added in Korea, specific detailed evaluation items are not presented. EGNOS, which is expected to be the most compatible with KASS and is being serviced after its development, has already been evaluated. In this paper, we analyze the regulations applied to EGNOS construction and analyze the criteria of ground and flight test evaluation items required for flight testing, which is expected to be referenced to the flight inspection process in the future.

Data Load Process of large-sized media for avionics using FTP and JSON (FTP와 JSON을 활용한 대용량 미디어의 항공장비용 데이터 로드 프로세스)

  • Ji-Hwan Choi;Nak-Min Choi;Jae-Kwon Shin
    • Journal of Advanced Navigation Technology
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    • v.27 no.5
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    • pp.610-620
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    • 2023
  • The interest in the aircraft interior market is gradually growing due to technological development based on the 4th industrial revolution and competition for airlines to attract customers, and as part of that, Cabin Display System (CDS) for FAA Part.25 civil aircraft is being developed in Korea. The CDS is a system that provides various multimedia services to passengers by utilizing Flexible and Transparent Organic Light Emitting Diodes (OLED) with Integrated Display Processing Module (IDPM). This paper presents a new method for efficient Data Load Process of large-sized files and deals with their implementation and performance. The results of this study are expected to be applied to Data Load Process development of avionics that require reliable large-capacity file transmission along with reducing the costs of development compared to existing ARINC-615A.

A Study on Implementation Trend of Aviation System Block Upgrades(1) (ICAO의 ASBU(Aviation System Block Upgrades) 추진 동향(1))

  • Park, Bomi;Kim, Jun-hyuk
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.24 no.2
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    • pp.74-80
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    • 2016
  • Development of air navigation and avionics technologies led to solve the problems that conventional ATM system had. The International Civil Aviation Organization developed the Aviation System Block Upgrades (ASBU) initiative in order to harmonize global ATM planning and technology upgrades and urged to implement the recommendations for the member States. The ASBUs provide the road map to assist air navigation service providers in the development of their individual strategic plans and investment decisions. In this paper, the operational concepts in 2 performance improvement areas, Airport Operations and Globally Interoperable System and Data in ASBUs, have been summarized. In Airport Operations area the new management technologies and required systems are presented for optimizing the traffic flow in airport area and terminal airspace. Data format standards and required systems presented for information integration and usage of the new system under Globally Interoperable System and Data area.

Design and Implementation of High-availability System (임무컴퓨터를 위한 고가용 시스템의 설계 및 구현)

  • Jeong, Jae-Yeop;Lee, Cheol-Hoon
    • Proceedings of the Korea Contents Association Conference
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    • 2008.05a
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    • pp.529-533
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    • 2008
  • Mission Computer performs important role both managing a whole system and dealing with a specific mission in avionics system. In general, the fault of SPOF(Single Point Of Failure) in unity system can lead to failure of whole system. It can cause a failure of a mission and also can threaten to the life of the pilot. So, in this paper, we design the HA(High-availability) system so that dealing with the failure. And we use HA software like Heartbeat, Fake, DRBD and Bonding to managing HA system.

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The Development and Performance Evaluation of Adaptive Monitoring sensor for the Marine IT System (해양 IT시스템용 적응형 모니터링 센서의 개발 및 성능 평가)

  • Cho, Jeong-Hwan;Roh, Hee-Jung
    • Journal of the Korean Institute of Illuminating and Electrical Installation Engineers
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    • v.29 no.6
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    • pp.90-95
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    • 2015
  • This paper proposes the new adaptive gain control monitoring sensor for the marine IT system. The marine IT system sensors make it possible to conduct search missions, record climate changes, provide pollution control, study marine life, conduct survey missions, tactical surveillance, and predict natural disturbances in the ocean. In this paper, the adaptive gain control circuit which changes its parameters according to the ambient noise situation for obtaining the precise location information of marine IT system sensor is developed and analyzed. The performance characteristics for ensuring the precise location information of marine system sensor is presented and analyzed. The theoretical and experimental studies have been carried out. The presented results from the above investigation show considerably excellent performance for the monitoring of the marine system.

Performance of Full Duplex Switched Ethenlet Systems with a Dual Traffic Regulator for Avionic Data Buses (이중 트래픽 조절기능이 있는 항공데이터버스용 전이중 이더넷 교환시스템의 성능 분석)

  • Kim, Seung-Hwan;Yoon, Chong-Ho;Park, Pu-Sik
    • Journal of the Institute of Electronics Engineers of Korea TC
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    • v.46 no.2
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    • pp.89-96
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    • 2009
  • As increasing the number of digital control devices installed on aircrafts and their transmission speed, various digital data buses have been introduced to provide reliable and high-speed characteristics. These characteristics of avionics data bus are highly related on the fault-tolerant performance which can make minimize jitter and loss during data transfer. In this paper, we concerned about a new traffic shaping scheme for increasing the reliability of Avionics Full Duplex Switched Ethernet (AFDX) systems based on ARINC 664 standard. We note that the conventional AFDX with a single regulator per virtual link system may produce aggregated traffics as the number of virtual links increasing. The aggregated traffic results in large jitters among frames. To remedy for the jitter and loss of data, we propose a dual regulator scheme for the AFDX system. The purpose of the additional regulator is to additionally regulate aggregated traffics from a number of per virtual link regulators. Using NS-2 simulator, we show that the proposed scheme provides a better performance than the single regulator one. It is worthwhile note that the proposed AFDX with Dual Regulator scheme can be employed to not only aircraft networks but other QoS sensitive networks for robot and industrial control systems.

Implementation of Flight Data Storage System with Compression and Security (압축 및 보안 기능이 있는 비행데이터 저장 시스템 구현)

  • Cho, Seung-Hoon;Ha, Seok-Wun;Moon, Yong-Ho
    • IEMEK Journal of Embedded Systems and Applications
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    • v.7 no.3
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    • pp.157-162
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    • 2012
  • In this paper, we propose a flight data storing system for effective data processing. Since the flight data contains critical information and their sizes are vast, encryption and compression would be needed to manage the flight data in effect. And we implemented the flight data storing system using an embedded board with DSP based on DPCM compression and AES encryption. Especially, we applied the reordering technique to advance the security function. From the simulations for two type data of voice and avionics, we found the developed system is well performed.

Smoke Detection System Research using Fully Connected Method based on Adaboost

  • Lee, Yeunghak;Kim, Taesun;Shim, Jaechang
    • Journal of Multimedia Information System
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    • v.4 no.2
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    • pp.79-82
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    • 2017
  • Smoke and fire have different shapes and colours. This article suggests a fully connected system which is used two features using Adaboost algorithm for constructing a strong classifier as linear combination. We calculate the local histogram feature by gradient and bin, local binary pattern value, and projection vectors for each cell. According to the histogram magnitude, this paper applied adapted weighting value to improve the recognition rate. To preserve the local region and shape feature which has edge intensity, this paper processed the normalization sequence. For the extracted features, this paper Adaboost algorithm which makes strong classification to classify the objects. Our smoke detection system based on the proposed approach leads to higher detection accuracy than other system.

Generation of System Requirements for Smart UAV (스마트 무인기 시스템 요건 도출)

  • Lee, Jung Jin
    • Journal of the Korean Society of Systems Engineering
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    • v.1 no.1
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    • pp.32-38
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    • 2005
  • This paper presents the brief generation process of system requirements for Smart UAV from a development objective. The current Smat UAV requirements deal with the restricted life cycle from development to test and verification exclusive of full life cycle because of the new technology demonstration research program funded by governments. The Smart UAV system consists of flight vehicle, avionics, communication link, payload, ground control station and ground supporting system. In this paper, top-down flown requirements are introduced how to allocate to each sub-system.

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The Design of a Fault Tolerant Store Management System

  • Lee, Dongho;Park, Hansol
    • Journal of the Korea Society of Computer and Information
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    • v.20 no.10
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    • pp.1-5
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    • 2015
  • Based on the dual hardware and software with distributed recovery blocks, the centralized type fault tolerant store management system(SMS) was proposed. As a result of trade off study related to mutiplex hardware system design, dual single board computer(SBC) was adapted. To verify redundancy function of the proposed structure, the prototype SMS and weapon simulator were used. The proposed SMS operated normally without being affected by a primary SBC failure. The switching time from primary SBC to shadow SBC was within 200 ms. The reliability of the proposed SMS was predicted and compared with the non fault tolerant SMS, thereby it was proved that the proposed SMS has a higher reliability than the non fault tolerant system within effective range.