• Title/Summary/Keyword: 항법소프트웨어

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Operational Concept for the Software Product Line Framework of Navigation Software (항법소프트웨어 Software Product Line 프레임워크 운영개념)

  • Park, Samjoon;Noh, Sungkyu;Kim, Dohyung;Lee, Sunju;Park, ByungSu;Lee, Inseop
    • KIPS Transactions on Software and Data Engineering
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    • v.10 no.6
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    • pp.201-210
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    • 2021
  • Navigation Software for the various weapon systems has common functionalities which give the possibility of common use among them. SPL(Software Product Line) framework of the navigation software for weapon system refers to developing a standardized navigation software platform from common functionalities of navigation software, managing the standardized navigation software platform, and developing weapon system navigation software such as navigation software for missile, UAV(Unmanned Air Vehicle), submarine, and etc. from the standardized navigation software platform. In this paper, we propose SPL based navigation software development process, Integrated Development Environment and operational concept of SPL framework. The operational concept will be defined by specifying the role of every stake holders and their activity scenario. The Operational concept would be referenced to implement SPL for other domain through using with detail implementation guide.

다중 기준국에서의 위성신호 이상감시 소프트웨어 설계 및 구현

  • Hong, Cheol-Ui;Jo, Deuk-Jae;Park, Sang-Hyeon;Yu, Yun-Ja;Sin, Mi-Yeong
    • Proceedings of the Korean Institute of Navigation and Port Research Conference
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    • 2011.11a
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    • pp.196-197
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    • 2011
  • 신뢰성 있는 위성합법기반의 위치정보 서비스 제공을 위해서는 오차정보서비스와 항법신호의 이상을 감시하는 서비스가 요구된다. 항법신호 이상감시는 그동안 단일 기준국에 대한 연구 위주로 진행되어 왔다. 본 연구에서는 단일 기준국이 아닌 다중 기준국을 기반으로 한 항법신호 이상을 감시하기 위한 소프트웨어를 설계하고 구현하는데 그 목적이 있다. 다중 기준국을 기반으로 한 항법신호 이상감시 소프트웨어는 GPS 메시지를 효과적으로 수집하는 수집부와, 수집된 데이터를 이용하여 다중 기준국에서의 항법신호를 감시하기 위한 알고리즘 처리부로 나누어 소프트웨어의 효과적인 동작을 위해 모듈화를 진행하였으며, 시스템에 대한 안정성 및 확장성을 고려하여 설계하였다. 본 연구를 통하여 단일 기준국에서는 확인할 수 없는 항법신호 이상을 정밀하게 탐지할 수 있게 되었으며, 오차정보 서비스를 제공하는데 있어 기반자료로 활용될 수 있다.

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Requirement Analysis and Conceptual Design of GNSS Digitized IF Signal Simulator (위성항법 이산화 IF 신호 시뮬레이터 요구사항분석 및 개념 설계)

  • Lee, Sang-Uk;Ju, In-Won;Lee, Jae-Eun
    • Journal of Satellite, Information and Communications
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    • v.2 no.1
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    • pp.41-47
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    • 2007
  • Software GNSS digitized IF signal simulator is being developed by ETRI as a part of development of software-based GNSS Test & evaluation Facility which will provide test and evaluation environment for various software level application and navigation algorithm in GNSS. Software GNSS IF signal simulator will provide digitized GNSS signal including GPS and Galileo. The requirement analysis and conceptual design for the Software GNSS IF signal simulator is presented in this paper.

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Block Correlator for Real-Time GPS L1 Software Receiver (소프트웨어 기반의 실시간 GPS L1 수신기를 위한 블록 상관기)

  • Kim, Tae-Hee;Lee, Sang-Uk
    • Journal of Satellite, Information and Communications
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    • v.6 no.1
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    • pp.80-85
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    • 2011
  • In this paper, a software-based real-time GPS L1 receiver is proposed for the block correlation techniques. Recently various navigation satellite navigation receivers in the environment for the development of more efficient software-based real-time receiver need to be developed. It is composed of components such as signal supplier, signal acquisition, signal tracking, navigation data processing, and navigation solution. They are designed and implemented as component based software for enhancing reusability and modifiability for user to have more flexibility during development of receiver. This paper will describe design, implementation, and verification of the developed realtime software GNSS receiver.

Alignment and Navigation of Inertial Navigation and Guidance Unit using Inertial Explorer Software (Inertial Explorer 소프트웨어를 이용한 관성항법유도장치 정렬 및 항법계산)

  • Kim, Jeong-Yong;Oh, Jun-Seok;Roh, Woong-Rae
    • Aerospace Engineering and Technology
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    • v.9 no.1
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    • pp.50-59
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    • 2010
  • In this paper, the alignment and navigation results by INGU(Inertial Navigation and Guidance Unit) onboard software and by Inertial Explorer which is a post-processing software specialized for IMU(Inertial Measurement Unit) are compared for identification of inertial sensor error models and estimation of alignment and navigation errors for KSLV-I INGU. For verification of the IMU error estimated by Kalman Filter of Inertial Explorer, the covariance parameters of inertial sensor error model state are identified by using stochastic error model of inertial sensors estimated by Allan variance and the alignment and navigation test with static condition and the land navigation test with dynamic condition are carried out. The validity of inertial sensor model for KSLV-I INGU is verified by comparison the alignment and navigation results of INGU on-board software and Inertial Explorer.

Development of MATLAB GUI-based Software for Performance Analysis of RNSS Navigation Message and WAD-RNSS Correction (지역 위성항법시스템 항법메시지 및 광역 보정정보 성능 분석을 위한 MATLAB GUI 기반 소프트웨어 개발)

  • Jaeuk Park;Bu-Gyeom Kim;Changdon Kee;Donguk Kim
    • Journal of Advanced Navigation Technology
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    • v.27 no.5
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    • pp.510-518
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    • 2023
  • This paper introduces a MATLAB graphical user interface (GUI) based software for performance analysis of navigation message and wide area differential correction of regional navigation satellite system (RNSS). This software was developed to analyze satellite orbit/clock-related performance of navigation message and wide area differential correction simulating RNSS for regions near Korea based on different distributions of monitor and reference stations. As a result of software operation, navigation message and wide area differential correction are given as output in MATLAB file format. From the analysis of output, it was confirmed that valid navigation message and wide area differential correction could be generated from the results about statistical feature of orbit and clock prediction errors, cm-level fitting errors for navigation message parameters, and 81.9% enhancement in range error for wide area differential correction.

Design of a Testable SDINS/GPS Integrated Navigation Software Structure of UML Based (테스트 가능한 UML 기반의 SDINS/GPS 통합 항법 소프트웨어 구조 설계)

  • Cho, Sung-Lyong;Park, Sul-Gee;Kang, Hee-Won;Lim, Deok-Won;Hwang, Dong-Hwan;Lee, Sang-Jeong
    • Proceedings of the KIEE Conference
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    • 2009.07a
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    • pp.1923_1924
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    • 2009
  • 최근 들어 소프트웨어의 테스트에 대한 필요성이 증가함에 따라 소프트웨어 테스트 방법에 대한 연구가 활발해지고 있으며 이를 적용한 제품들도 다양한 분야에서 개발되고 있다. 또한 UML과 같은 모델 기반의 언어가 등장함에 따라 소프트웨어의 재사용성 등을 높일 수있는 설계가 가능하다. 본 논문에서는 테스트가 가능한 SDINS/GPS 통합 항법 소프트웨어 구조를 UML 모델로 제시하며, 제시한 모델에 대한 테스트 절차를 기술한다. 본 논문의 결과를 이용하여 SDINS/GPS 통합 항법 소프트웨어를 설계하면 소프트웨어를 다른 하드웨어로 이식하는 것과 다른 센서 측정치를 처리하기 위한 소프트웨어 확장이 용이하다.

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Development of the Avionics System Software for Flight Simulator Using Navigation Geography Database (항법 지리 데이타베이스를 이용한 비행 시뮬레이터용 항공전자 장치 소프트웨어 개발)

  • Baek, Joong Hwan
    • Journal of Advanced Navigation Technology
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    • v.1 no.1
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    • pp.59-69
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    • 1997
  • In this paper, we construct a navigation geography database using R-tree, and develop a software for avionics systems such as VOR, ILS, DME, and NDB. First, we design the navigation geography database using R-tree, and construct a database for navigation aids facilities of every airport. In order to implement avionics software, we develop some calculating algorithms for distance, bearing, and deviation angle between an aircraft and a VOR station for VOR, and deviation angle from a LLZ, glide slope from a GP, and range of markers for ILS. The navigation geography database system is composed of map data manager which can construct and update the database, real-time searcher which provides information about the avionics system, geography database, and user interface.

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복합 지상항법 장치의 성능 분석을 위한 전산 모의 소프트웨어 개발

  • Gwon, Cheol-Beom;Kim, Sang-Sun;Park, Won-Jang;Hong, Jin-Seok;Song, Jin-U;Park, Yeong-Beom
    • Proceedings of the Korean Institute of Navigation and Port Research Conference
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    • v.2
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    • pp.537-540
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    • 2006
  • 항법 장치의 특성을 이해하고 통합 필터를 설계하기 위한 기본 도구로 많이 활용되는 것이 시뮬레이션 도구이다. 이것은 실재 시스템을 구현할 때 부딪히는 각종 어려움으로부터 벗어나, 비교적 쉽게 성능분석을 할 수 있다는 장점 때문이다. 본 논문에서는 윈도우 기반의 전산 모의 소프트웨어를 개발하고, 이 프로그램을 이용하여 GPS와 INS 등의 센서를 이용한 복합 지상항법 시스템의 성능을 분석하였다.

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A Scoping Method to Implement Software Product Line for Inertial Navigation System (관성항법소프트웨어 SPL(Software Product Line) 구현을 위한 플랫폼 범위결정 기법)

  • Park, Samjoon;Noh, Sungkyu;Lee, Kwanwoo;Park, ByungSu;Nam, Seongho
    • KIPS Transactions on Software and Data Engineering
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    • v.10 no.7
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    • pp.251-256
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    • 2021
  • Software Product Line Engineering (SPLE) has been known as an efficient and effective software reuse methodology. One of the key activities of SPLE is scoping analysis, which determines the range of the features to be developed as reusable assets. Although several scoping methods has been reported, they are not sufficient to apply them to the defense domain. In this paper, we present a scoping method applicable to the defense domain, and present a case study for applying SPLE to inertial navigation weapon system. At first, the proposed method determines the range of candidate features to be applied for the platform. The range is then adjusted from the perspective of product benefit. The final range of features is decided through considering the total cost of a product line. We will demonstrate and evaluate the applicability of the proposed method by showing how we can decide the scope of features to be engineered for the navigation software product line.