• 한국우주과학회:학술대회논문집(한국우주과학회보)
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• 한국우주과학회 2006년도 한국우주과학회보 제15권1호
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• pp.125-128
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• 2006

한국항공대학교 우주시스템 연구실에서 개발 중인 25kg급 나노위성, HAUSAT-2의 통신 서브시스템을 설계 및 제작하고, 시험을 통하여 성능을 검증하였다. HAUSAT-2의 통신 서브시스템은 임무 수행을 위해 지상국의 명령을 수신하고, 위성의 상태 정보와 임무 자료를 지상국으로 송신하는 역할을 담당하도록 설계하였으며, 위성 시스템의 특성을 고려하여 높은 신뢰성을 갖도록 제작되었다. 본 논문에서는 HAUSAT-2 통신 서브시스템의 시험모델(Engineering Model) 설계, 제작 및 시험결과를 기술하였다.

• 항공우주시스템공학회지
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• 제1권4호
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• pp.13-21
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• 2007

As one of YHF digital data link technologies, VDL Mode 2 is designed to be an air-to-ground subnetwork of the Aeronautical Telecommunication Network (ATN) based on the Open System Interconnection (OSI) architecture. VDL Mode 2 can be used in ATS Applications especially for CPDLC and ADS. And it is also expected to replace ACARS (Aircraft Communications Addressing and Reporting System) which has broadly been used in AOC for over 20 years. This paper presents the design result of VDL Mode 2 system under AOA (ACARS Over AVLC) environment for the implementation of bit-oriented ATS applications. The system is composed of airborne and ground subsystem. Airborne subsystem consists of VDR, CMU and an aircraft test equipment with CPDLC/ADS client applications for operational test and ground system consists of Ground Station which includes ground VDR and ground communication controller, simple DSP (Datalink Service Processor) and a ground test equipment with CPDLC/ADS server applications.

• 한국항공우주학회지
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• 제41권11호
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• pp.921-930
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• 2013

(주)쎄트렉아이는 고해상도 전자광학카메라인 EOS-D Ver.1.0의 개발 및 검증을 성공적으로 완료하였다. EOS-D Ver.1.0 시스템은 기존 EOS-C 계열 대비 향상된 공간 해상도 및 방사학적 해상도를 갖도록 설계되었다. EOS-D Ver.1.0의 열제어계는 능동 열제어 방식과 수동 열제어 방식을 혼용하여 개발되었다. 또한, 광학계 주구조물의 수분 발산 효과에 의한 비정렬 상태를 보상할 수 있도록 초점 조절장치(refocusing mechanism)를 설계하고 이를 검증하였다. 설계를 바탕으로 실제 모델을 제작, 인증 수준의 열진공 시험을 통해 설계 여유(design margin)와 작업도(workmanship)를 확인하였다. 또한 열-수치 모델(TMM)에 대한 검증 작업을 수행하여 해석 모델이 실제 모델의 열적 특성을 잘 모사하고 있음을 확인하였다.

• 한국신뢰성학회지:신뢰성응용연구
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• 제18권3호
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• pp.201-207
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• 2018

Purpose: To develop the reliability growth planning for a subsystem of guided weapon system using PM2-Continuous model. Methods: The target MTBF of the subsystem is set by allocating the system target MTBF to the lower level, where ARINC method is applied. Other model parameters such as initial MTBF, management strategy ratio and average fix effectiveness factor are chosen from historical growth parameter estimates. Given the values of model parameters, the reliability growth planning curve using PM2-Continuous model is constructed and the sensitivity analyses are performed for the changes of model parameters. Results: We have developed the reliability growth plan for a subsystem of guided weapon system using PM2-Continuous model. It was found that the smaller the ratio of initial MTBF to target MTBF, the smaller the management strategy ratio, the smaller the average fix effectiveness factor, and the shorter the development test period, the higher reliability growth is required. Conclusion: The result of this study will be used as a basis for establishing the reliability growth plan, the test period setting and the budget appropriation for the similar system entering the system development stage in the future.

• 천문학논총
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• 제24권1호
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• pp.65-81
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• 2009

We present the performance test results of VLBI Correlation Subsystem (VCS) trial product which was being developed for 1 year from August 2007. It is a core component of Korea-Japan Joint VLBI Correlator (KJJVC). The aim for developing VCS trial product is to improve the performance of VCS main product to reduce the efforts and cost, and to solve the design problems by performing the preliminary test of the manufactured trial product. The function of VCS trial product is that it is able to process the 2 stations-1 baseline, 8 Gbps/station speed, 1.2 Gbps output speed with FX-type. VCS trial product consists of Read Data Control Board (RDC), Fourier Transform Board (FTB), and Correlation and Accumulation Board (CAB). Almost main functions are integrated in the FTB and CAB board. In order to confirm the performance of VCS trial product functions, the spectral analysis, delay compensation and correlation processing experiments were carried out by using simulation and real observation data. We found that the overflow problem of re-quantization after FFT processing was occurred in the delay compensation experiment. We confirmed that this problem was caused by valid bit-expression of the re-quantized data. To solve this problem, the novel method will be applied to VCS main product. The effectiveness of VCS trial product has been verified through the preliminary experimental results, but the overflow problem was occurred.

• 대한원격탐사학회지
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• 제18권1호
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• pp.53-59
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• 2002

The MSC is a payload on the KOMPSAT-2 satellite to perform the earth remote sensing. The instrument images the earth using a push-broom motion with a swath width of 15 km and a GSD(Ground Sample Distance) of 1 m over the entire FOV(Field Of View) at altitude 685 km. The instrument is designed to haute an on-orbit operation duty cycle of 20% over the mission lifetime of 3 years with the functions of programmable gain/offset and on-board image data compression/storage. The MSC instrument has one channel for panchromatic imaging and four channel for multi-spectral imaging covering the spectral range from 450nm to 900nm using TDI(Time Belayed Integration) CCD(Charge Coupled Device) FPA(Focal Plane Assembly). The MSC hardware consists of three subsystem, EOS(Electro Optic camera Subsystem), PMU(Payload Management Unit) and PDTS(Payload Data Transmission Subsystem) and each subsystems are currently under development and will be integrated and verified through functional and space environment tests. Final verified MSC will be delivered to spacecraft bus for AIT(Assembly, Integration and Test) and then COMSAT-2 satellite will be launched after verification process through IST(Integrated Satellite Test). In this paper, the introduction of MSC, the configuration of MSC electronics including electrical interlace and design of CEU(Camera Electronic Unit) in EOS are described. MSC Operation parameters induced from the operation concept are discussed and analyzed to find the influence of system for on-orbit operation in future.

• 한국항공우주학회지
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• 제42권8호
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• pp.674-682
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• 2014

RFTS(Radio Frequency Test Set)은 저궤도 위성과 정지궤도 위성의 AI&T 기간 동안 TC&R RF 서브시스템을 검증하는 필수 장비이다. 본 논문에서는 새로운 RFTS의 상세 설계 내용을 제시하는데 기존의 RFTS와 달리 위성 프로젝트 별 시험 수행 시 수정 없이 바로 적용할 수 있도록 하였다. 하드웨어와 소프트웨어는 이를 만족하도록 설계 되었고 기능 별 모듈화와 상용품 사용의 확장으로 보다 손쉬운 제어와 운용이 될 수 있도록 하였으며 시스템의 신뢰성 향상을 가져오도록 하였다. 또한 보다 정확한 기준 클락을 채택하여 RF 측정에 대한 신뢰도를 높였다.

• 한국철도학회:학술대회논문집
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• 한국철도학회 1999년도 추계학술대회 논문집
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• pp.202-208
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• 1999

Train system like high speed train is assemble by a number of subsystem. Therefore, the Integration of train system needs the process that investigates the interface and influence between subsystems. In this paper, It studied the Design & Integration and major process of Korea High Speed Tram Project,

• 가족자원경영과 정책
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• 제2권1호
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• pp.59-77
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• 1998

The purpose of this study was to test a causal model of subjective financial well-being. The data of this research was obtained from 660wives who lived in Seoul, 1996. Major findings of this study were at follows: 1. Both employed and unemployed wives, younger managers were more likely to have a higher cohesion and adaptability between spouses. For the unemployed wives, locus of control over managers’financial situation and perception of gap between standard and level of living were significant predictors of the personal subsystem. 2. In both groups, financial planning was positively influenced by amount of saving. But amount of saving was not significant predictor of financial implementing. Financial implementing was positively influenced by locus of control, in the unemployed wives. For the employed wives, predictors of financial implementing were family income and marriage duration. 3. For the employed wives, the effect of personal and managerial subsystem on subjective financial well-being was greater than unemployed wives. 4. It was found that personal and managerial subsystems had effect on subjective financial well-being. Thus, the path model designed in this research was found to be proven for employed and unemployed wives.

• 대한기계학회논문집A
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• 제25권5호
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• pp.834-840
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• 2001

A real time multibody vehicle dynamics model has been developed and implemented using a subsystem synthesis method based on recursive formulation. To verify real time simulation capability the developed model has been applied to HMMWV(High Mobility Multipurpose Wheeled Vehicle) with steering system. For the kinematically driven steering system, the coupled front suspension-steering subsystem can be decoupled into two SLA suspension subsystems, which improves the efficiency of simulation. To investigate theoretical efficiency, operational counting method has been also employed to compare the proposed model with the conventional recursive dynamics model. Various simulations such as unsymmetric bump run, step steering(J-turn) and sine steering input test have been carried out to verify the real time feasibility of the proposed model.