• Proceedings of the Safety Management and Science Conference
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• 2001.05a
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• pp.77-81
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• 2001

Burn-in is a test procedure to find and eliminate the inherent initial failure of a product during or at the final stage of production process. Software testing is the validation and verification process which is used to cut off the faults from a software. The two have the common function and objective of "debugging". This article summarizes some significant models on the optimal hardware and software burn-in time, and provides the relevant paper lists. The need for the development of the unified burn-in policy of a hardware-software system is addressed.addressed.

• Journal of Korean Society of Industrial and Systems Engineering
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• v.19 no.38
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• pp.61-68
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• 1996

Quality Assurance Principles must be effectively implemented in developments and in use of safety critical software in nuclear industry. Brief definitions related to computer software and quality assurance were defined and several methods for evaluating software quality were proposed herewith. Independent verification and validation was suggested to assure the quality of safety critical software.

• The Transactions of The Korean Institute of Electrical Engineers
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• v.64 no.2
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• pp.331-337
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• 2015

The power flow analysis of electrified railway is required complicated calculation, because of variable load. Train runs trough rail supplied by electric power therefore, the load value in electrified railway system fluctuates along time. The power flow algorithm in electrified railway system is different from general power system, and the power flow simulation is peformed by the particular simulation software. Powerail is simulation software for analysis of traction power supply system developed by KRRI, in 2008. This consists of load forecasting module, including TPS and time scheduling, and power flow module. This software was verified by measured current under normal feeding condition, however, has not been verified by voltage on the condition of extended feeding. This paper presents the verification of PowerRail based on voltage drop under extended feeding condition. This is performed by comparing simulation result with field test. Field test and simulation is done in commercial railway line.

• Proceedings of the IEEK Conference
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• 2003.07b
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• pp.1007-1010
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• 2003

This paper presents in-circuit system-on-chip verification and debugging environment. To maximize the emulation speed, the software part is compiled natively for the host computer and the hardware part is mapped into FPGA. The two parts communicate with each other in transaction level. The operation of the hardware part and the software part is recorded independently during the emulation, and after the emulation is over, they are merged in a waveform to give user a unified view that covers both hardware and software.

• Journal of Institute of Control, Robotics and Systems
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• v.10 no.10
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• pp.956-960
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• 2004

The Vehicle Dynamic Simulator(VDS) is a key equipment of the performance verification of attitude control subsystem and it simulates the real dynamic environment that spacecraft undergoes during mission operation. All the software models and hardware interfaces necessary for the closed-loop simulation of the spacecraft dynamics are implemented. Using VDS, KOMPAT-2 attitude control logic functions and performance was verified. In this paper, the hardware and software configurations of KOMPSAT-2 VDS was described briefly and the information flow and exchanges between software models and actual hardwares during close loop simulation was described in the systematic point of view.

• Proceedings of the Korean Information Science Society Conference
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• 2003.10c
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• pp.547-549
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• 2003

위성의 개발 및 제작에는 많은 비용과 기간이 소요되며. 일반적으로 사용되는 장비들과는 전혀 다른 우주환경에서 임무를 수행하게 된다. 그리고 위성의 경우에는 발사이후에 발생하는 오류들을 수정하는 것이 거의 불가능하므로 위성의 성공적인 임무완수를 위해서는 철저한 사전검증 작업들이 필요하게 된다. 특히, 위성의 궤도, 자세를 제어하고 실제적인 임무수행을 관할하는 위성탑재소프트웨어에 대한 완벽한 검증이 필요하다. 이러한 소프트웨어의 통합 및 조립시험. 검증시험을 위해 저궤도 위성의 FSW(Flight Software) 개발단계에서 실제 위성시스템과 유사한 인터페이스를 제공하는 개발도구인 STB(Software Test Bed)가 제작되며, 제작된 STB를 통한 FSW의 검증시험 및 분석을 지원하기 위한 구문분석프로그램으로 VTSP(Verification Test Script Parser)를 개발하게 된다. 본 논문에서는 이러한 STB와 VTSP에 대한 전반적인 소개와 함께 개발된 STB와 VTSP를 이용하여 실제 위성탑재소프트웨어를 검증하기 위한 시험환경에 대해 알아보고자 한다.

• Proceedings of the Korean Information Science Society Conference
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• 2002.10e
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• pp.430-432
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• 2002

다목적실용위성 2호 FSW(Flight Software)의 개발단계에서 통합 및 시험, 검증시험을 위해 실제 위성시스템과 유사한 인터페이스를 제공하는 개발도구인 STB(Software Test Bed)가 제작되었으며, 제작된 STB를 통한 FSW의 검증시험 및 분석을 지원하기 위한 프로그램으로서 구문분석 프로그램을 이용한 VTSP(Verification Test Script Parser)의 개발이 필요하다. 본 논문에서는 구문분석 도구인 FLEX와 BISON을 이용하여 FSW가 실제시스템 상에서 요구조건에 따라 수행되고 있는지를 자동적으로 검증하기 위해 C 언어와 유사한 사용법을 가지며, 다양한 검증시험 환경에 적합한 VTSP를 개발하기 위한 전체적 개발환경 및 VTSP의 기능에 대해 소개한다.

• Journal of the Korea Society of Computer and Information
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• v.27 no.12
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• pp.209-217
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• 2022

Naval CMS(Combat Management System) is linked to various sensors and weapon equipment and use DDS(Data Distribution Service) for efficient data communication between ICU(Interface Control Unit) Node and IPN(Information Processing Node). In order to use DDS, software in the system communicates in an PUB/SUB(Publication/Subscribe) based on DDS topic. If the DDS messages structure in this PUB/SUB method does not match, problems such as incorrect command processing and wrong information delivery occur in sending and receiving application software. To improve this, this paper proposes a DDS message structure integrity verification method. To improve this, this paper proposes a DDS message structure integrity verification method using a hash tree. To verify the applicability of the proposed method to Naval CMS, the message integrity verification rate of the proposed method was measured, and the integrity verification method was applied to CMS and the initialization time of the existing combat management system was compared and the hash tree generation time of the message structures was measured to understand the effect on the operation and development process of CMS. Through this test, It was confirmed that the message structure verification method for system stability proposed in this paper can be applied to the Naval CMS.

• Journal of the Korea Society for Simulation
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• v.27 no.1
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• pp.25-32
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• 2018

This paper presents an efficient software reliability testing method for the model based auto-generated code and reify a dynamic test procedure. The benefits of executing the model-based each static/dynamic reliability test before the code-based static/dynamic reliability test are described. Also, The correlations of code/model based reliability test are demonstrated by using model testing tool, Model Advisor and Verification and Validation, and the code testing tool, PolySpace and LDRA. The result of reliability test is indicated in this paper.

• 제어로봇시스템학회:학술대회논문집
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• 2003.10a
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• pp.1465-1469
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• 2003

In general satellite verification process, the AOCS (Attitude & Orbit Control Subsystem) should be verified through several kinds of verification test which can be divided into two major category like FBT (Fixed Bed Test) and polarity test. And each test performed in different levels such as ETB (Electrical Test Bed) and satellite level. The test method of FBT is to simulate satellite dynamics with sensors and actuators supported by necessary environmental models in ETB level. The VDS (Vehicle Dynamic Simulator) try to make the real situation as possible as the on-board processor will undergo after launch. The purpose of FBT test is to verify that attitude control logic function and hardware interface is designed as expected with closed loop simulation. The VDS is one of major equipments for performing FBT and consists of software and hardware parts. The VDS operates in VME environments with target board, several commercial boards and custom boards based on the VxWorks real time operating system. In order to make time synchronization between VDS and satellite on-board processor, high reliable semaphore was implemented to make synchronization with the interrupt signal from on-board processor. In this paper, the real-time operating environment used on VDS equipment is introduced, and the hardware and software configurations of VDS summarized in the systematic point of view. Also, we try to figure out the operational concept of VDS and AOCS verification test method with close-loop simulation.