• Title/Summary/Keyword: Avionics System

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Test Plan for Anti-Jamming System Performance Evaluation

  • Park, Ji-Hee;Kwon, Seung Bok;Shin, Dong-Ho
    • Journal of Positioning, Navigation, and Timing
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    • v.4 no.1
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    • pp.17-23
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    • 2015
  • With the increase in the risk of GPS jamming, the development and application of anti-jamming GPS techniques have been actively performed. As the objective performance verification of developed techniques is important, equipment development for verification and discussion on anti-jamming performance test method and procedure have also been conducted. However, most tests are related to the specification of equipment and therefore detailed procedure of the performance verification of an anti-jamming system needs to be developed. In this study, requirements for anti-jamming performance verification were described, and test configurations and performance evaluation items depending on three kinds of test methods (lab test, basic outdoor test, and chamber test) were suggested for anti-jamming performance verification.

Design of Monitoring System based on IoT sensor for Health Management of an Elderly (고령자 건강관리를 위한 IoT 센서 기반의 모니터링 시스템 설계)

  • Park, Myeong-Chul;Lee, Hun-Kee
    • Proceedings of the Korean Society of Computer Information Conference
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    • 2020.07a
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    • pp.603-604
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    • 2020
  • 한국사회는 전통적인 대가족제도가 급속히 해체되고 저 출산 및 고령화로 인한 고령층의 1인 가정의 수가 급속히 증가하고 있는 추세이다. 고령자 1인 가구에 대한 다양한 서비스와 고도화가 필요한 이유이다. 본 연구에서는 1인 가정을 대상으로 IoT 기기를 통한 다양한 PHR 생체 신호와 환경정보을 수집하고 수집된 정보를 바탕으로 건강상태를 모니터링하는 시스템을 제안한다. 제안하는 시스템은 의료기기에서 제공되는 개방형 PHR 데이터의 융합으로 정보 분석 및 예측능력을 강화하고 고독사 상황파악 및 방지 프로그램을 이행할 수 있는 기본 인프라을 구축하고자 한다. 또한 중장년층의 미래에 대한 불확실성을 제거하고 사회복지서비스의 확대를 위한 정책적 과제의 논의적 목적을 가지고 있다. 본 연구의 결과물은 사회 소외 계층에 대한 서비스 확대와 국민의 의료환경 개선에 도움이 될 것으로 사료된다.

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Model-based Test Cases Generation Method for Weapons System Software (무기체계 소프트웨어의 모델 기반 테스트 케이스 생성 방법)

  • Choi, Hyunjae;Lee, Youngwoo;Baek, Jisun;Kim, Donghwan;Cho, Kyutae;Chae, Heungseok
    • Journal of the Korea Institute of Military Science and Technology
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    • v.23 no.4
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    • pp.389-398
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    • 2020
  • Test cases in the existing weapon system software were created manually by the tester analyzing the test items defined in the software integration test procedure. However, existing test case generation method has two limitations. First, the quality of test cases can vary depending on the tester's ability to analyze the test items. Second, excessive time and cost may be incurred in writing test cases. This paper proposes a method to automatically generate test cases based on the requirements model and specifications to overcome the limitations of the existing weapon system software test case generation. Generate test sequences and test data based on the use case event model, a model representing the requirements of the weapon system software, and the use case specification specifying the requirements. The proposed method was applied to 8 target models constituting the avionics control system, producing 30 test sequences and 8 test data.

Filter design for protecting signal interference between RF equipments on aircraft (항공기 RF 장비들의 신호 간섭 방지를 위한 필터 설계)

  • Kim, Junhyoung;Kim, Bong-Gyu;Jeon, Young-Gu;Lee, Seong-Woo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.41 no.3
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    • pp.246-252
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    • 2013
  • This paper presents method to suppress signal interference by using the filter in the RF output stage of the radiation equipment as a way to avoid interference between the RF(Radio Frequency) equipment mounted on aircraft. Especially filter design to suppress harmonics of the radiation equipment and testing method to verify the filter's performance is presented. Filter was installed at RF output stage of U/VHF radio in order to prevent interference between U/VHF(Ultra/Very High Frequency) radio and data link system. Filter design and testing method in this paper will be able to give help in the design of aircraft equipments as a tool that can be used to establish measures for problem of interference in the aircraft.

A Stress Analysis for Pressure Vessel to Prevent Spontaneous Ignition of Coal Stockpile (저탄장 자연발화 방지를 위한 압력용기의 응력 해석)

  • Kim, Young In;Kim, Seung Hun;Jie, Min-Seok;Yeum, Chan Sub;Choi, Won Hyuck
    • Journal of Advanced Navigation Technology
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    • v.22 no.3
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    • pp.205-212
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    • 2018
  • Spontaneous ignition is not only severe economic damage but also a typical plant damage caused by harmful gases generated during the fire. Because coal is porous, it causes oxygen to be absorbed in the amount of oxygen per unit weight of oxygen, resulting in low humidity and low thermal conductivity. The cause and effect of spontaneous ignition are very complex, so it is difficult to prevent it beforehand and once it is difficult to digest it, it is difficult to digest it. This study examines structural safety by conducting a structural analysis of the cooling ball system to prevent spontaneous combustion of coal stockpile plants and external pressures.

A Study of Optimization Approach for GPS Anti-Jamming System's Integration on Military Aircraft Based on the Requirement of Capability (요구성능 기반의 군용 항공기 항재밍 GPS 체계 구축 최적화 방안 연구)

  • Lee, Moongul;Shin, Kisu;Choi, Jaesik
    • Journal of the Korea Institute of Military Science and Technology
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    • v.18 no.1
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    • pp.66-83
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    • 2015
  • Global Positioning System(hereafter; GPS) is recently an essential element in the various navigation and weapon delivery systems of military aircraft. However, GPS is vulnerable to the jamming threats since its signal power is very weak. Therefore, ROK defense has been concerning how to resolve this issue and how to integrate these systems needed, and is trying to acquire the proper anti-jamming GPS system. This study is to provide several schemes against the jamming threats effectively. We propose the several processes to analyze the required capability and demonstrate the result's of modeling and simulations(hereafter; M&S) for this integration of military aircraft, and the mathematical programming model for system optimization of military aircraft anti-jamming GPS system on the basis analysis of M&S results which could be considered available budget and the project characteristic. These schemes will be helpful on proper acquisition of these systems and. We are looking forward to contributing to the integration of anti-jamming GPS system of ROK military aircraft.

Analysis of the Requirements and Design of KASS Measuring Equipment (KASS 탑재측정장비 요구사항 및 설계방안 분석)

  • Kim, Woo-Ri-Ul;Hong, Gyo-Young;Kang, Hee Won;Choi, Kwang-Sik
    • Journal of Advanced Navigation Technology
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    • v.21 no.6
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    • pp.544-548
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    • 2017
  • The International Civil Aviation Organization is recommending the use of SBAS on all aircraft by 2025 to urge PBN implementation around the world. As part of this, Korea is also developing KASS, a Korean SBAS. ICAO grants authority to the host nation aviation authority in the certification and operation of SBAS. The KASS system will be verified after detailed system design, fabrication and installation. In this paper, flight test parameters are derived from the flight inspection regulations and the configuration of the on - board measurement equipment for measuring the parameters has been proposed.

Analysis on the requirement of UMPC to construct the tactical datalink system (전술데이터 링크 시스템 구축에 필요한 항공기용 UMPC 요구 성능 분석)

  • Lim, Jun-Ho;Lee, Seoung-Pil
    • Journal of Advanced Navigation Technology
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    • v.14 no.5
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    • pp.604-609
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    • 2010
  • The tactical datalink system has been recognized as the key element in Network Centric Warfaret(NCW). The military has been putting great efforts into establishing datalink system using existing tactical radio and UMPC. but the aircraft operational environment and the requirement specification for equipments mounted in the avionics are differentiated with those in other platforms, so special efforts are needed to select suitable UMPC. In this paper, we consider the requirement analysis for UMPC in respect of processor performance, operation system (OS) and NVG compatibility. Additionally we have to make a effort to understand the operational environment of aircraft and examine th standard to select the appropriate UMPC, and then we expect to establish the tactical datalink system successfully.

Development of a Cooperative Heterogeneous Unmanned System for Delivery Services (물류수송을 위한 이종 협업 무인 시스템 개발)

  • Cho, Sungwook;Lee, Dasol;Jung, Yeondeuk;Lee, Unghui;Shim, David Hyunchul
    • Journal of Institute of Control, Robotics and Systems
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    • v.20 no.12
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    • pp.1181-1188
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    • 2014
  • In this paper, we propose a novel concept foran unmanned delivery service using a cooperative heterogeneous unmanned system consisting of a self-driving car and an unmanned aerial vehicle (UAV). The proposed concept is suitable to deliver parcels in high-density and high-rise urban or residential areas. In order to achieve the proposed concept, we will develop acooperative heterogeneous unmanned system. Customers can order goods using a smartphone application and the order information, including the position of the customer and the order time, and the package is transported automatically by the unmanned systems. The system assigns the tasks suitable for each unmanned vehicle by analyzing it based on map information. Performance is validated by experiments consisting of autonomous driving and flight tests in a real environment. For more evaluation, the landing position error analysis is performed using circular error probability (CEP).

Design of an FPGA-Based RTL-Level CAN IP Using Functional Simulation for FCC of a Small UAV System

  • Choe, Won Seop;Han, Dong In;Min, Chan Oh;Kim, Sang Man;Kim, Young Sik;Lee, Dae Woo;Lee, Ha-Joon
    • International Journal of Aeronautical and Space Sciences
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    • v.18 no.4
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    • pp.675-687
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    • 2017
  • In the aerospace industry, we have produced various models according to operational conditions and the environment after development of the base model is completed. Therefore, when design change is necessary, there are modification and updating costs of the circuit whenever environment variables change. For these reasons, recently, in various fields, system designs that can flexibly respond to changing environmental conditions using field programmable gate arrays (FPGAs) are attracting attention, and the rapidly changing aerospace industry also uses FPGAs to organize the system environment. In this paper, we design the controller area network (CAN) intellectual property (IP) protocol used instead of the avionics protocol that includes ARINC-429 and MIL-STD-1553, which are not suitable for small unmanned aerial vehicle (UAV) systems at the register transistor logic (RTL) level, which does not depend on the FPGA vender, and we verify the performance. Consequentially, a Spartan 6 FPGA model-based system on chip (SoC) including an embedded system is constructed by using the designed CAN communications IP and Xilinx Microblaze, and the configured SoC only recorded an average 32% logic element usage rate in the Spartan 6 FPGA model.