• Journal of Electrical Engineering and Technology
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• v.12 no.6
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• pp.2247-2255
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• 2017

Because the on-board charger (OBC) is installed in electric vehicles (EVs), high power density is regarded as a key technology. Among components of the OBC, inductors occupy more than 30% of the total volume. Thus, it is important to reduce the volume and the weight of inductors while maintaining thermal stability. Discontinuous conduction mode (DCM) can satisfy these requirements; however, only a few studies have adopted the DCM operation for OBCs because of the large inductor current ripple. In this paper, a design process is proposed for application of the DCM operation to OBCs. In order to analyze the inductor losses accurately, a numerical formula for the inductor current ripple is deduced based on a detailed analysis. Two inductors are fabricated using several ferrite cores and powder cores taking into consideration the inductor size, inductor losses, and temperature rise. In order to verify the analysis and design process, experimental results are presented that show that the designed inductors satisfy the requirements of the OBCs.

• Journal of Astronomy and Space Sciences
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• v.23 no.4
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• pp.445-452
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• 2006

In this paper, the conceptual design of satellite digital base put which is based upon data interface between satellite on-board computer and remote devices like satellite sub-components is presented. This conceptual design shows the unification of the interface between on-board computer and satellite remote devices and the hierarchical results of the interface level. A comparison of different system and merits and demerits of digital base part coming from this conceptual design is performed.

• Proceedings of the KIPE Conference
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• 2019.11a
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• pp.55-57
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• 2019

본 논문에서는 3.3[kW] on board charger(OBC)의 고전력 밀도 달성을 위한 LLC 공진형 컨버터의 최적 스위칭 주파수를 설계한다. 스위칭 주파수에 따라 달라지는 손실 양상 및 전력 밀도를 분석하기 위해 각 스위칭 주파수 별 반도체 소자 손실을 계산하고, 각 주파수에 적합한 변압기를 설계하여 주파수 변화에 따른 시스템 손실과 부피를 비교한다. 비교 결과를 바탕으로 최적 스위칭 주파수를 설계한다.

• Proceedings of the KIPE Conference
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• 2019.07a
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• pp.346-347
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• 2019

본 논문에서는 3.3 [kW] on-board charger (OBC) 용 phasw-shifted full-bridge (PSFB) 컨버터의 고효율 및 고전력 밀도 달성을 위한 스위칭 주파수 설계 방안을 제안한다. 스위칭 주파수에 따라 달라지는 손실 양상 및 전력 밀도에 대해 분석하기 위해 각 스위칭 주파수 별 반도체 소자 손실과 수동 소자 손실을 계산하고, 수동 소자의 부피 변화에 따른 전력밀도 변화를 분석한다. 분석 결과를 바탕으로 고효율 및 고전력밀도 달성을 위한 시스템 설계 포인트를 선정하고 시뮬레이션을 통하여 설계 결과를 검증한다.

• Aerospace Engineering and Technology
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• v.3 no.2
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• pp.20-24
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• 2004

In this paper, a pattern/position tolerance analysis is visited on the insert to mount spacecraft electronic equipment. SQP(Sequential Quadratic Programming) is used to obtain the position tolerance. For examples, the cases of RDU(Remote Drive Unit) and OBC(On Board Computer) in the KOMPSAT-2 STM(Structure and Thermal Model) are analyzed.

• Bulletin of the Korean Space Science Society
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• 2003.10a
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• pp.56-56
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• 2003

과학위성 1호의 OBC(On-Board Computer)와 Sybsystem 간, Subsystem간, 또는 위성과 지상국간의 통신이 가능해야한다. 그리고 OBC(On-Board-Computer)나 지상국에서의 위성의 모듈들을 명령(Command)을 통하여 제어할 수 있어야 한다. 또한 모듈들을 원격검침(Telemetry)을 통하여 상태를 확인할 수 있어야 한다. 위에서 언급한 기능을 수행하는 모듈이 바로 Network System이다 과학위성1호에는 총 6개의 Network System이 구현되었다. 각각의 Network System들은 여러 Subsystem들과 연결되어있고, Network System간에 또한 연결되어서 Subsystem간의 통신과 Network System에 연결된 모듈들을 제어하고 상태를 수집한다. 본 연구에서는 과학위성1호 Network System의 구조, 기능, Spec 및 연구 개발 내용을 소개한다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.32 no.1
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• pp.98-105
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• 2004

• Aerospace Engineering and Technology
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• v.13 no.2
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• pp.54-59
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• 2014

This paper cites about a test & analysis support set to support a testing and analysis of CFDP(CCSDS File Delivery Protocol) that processes commands and data as a series of file for reliable deep space communication. And this paper includes a basic description of CFDP and an objective and functions of CFDP-TASS(CFDP - Test Analysis & Support Set). CFDP-TASS is an equipment to examine OBC(On-Board Computer) CFDP in normal and abnormal cases, gather all packets in test, and support to analyze effectively the result of tests.

• Bulletin of the Korean Space Science Society
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• 2004.10b
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• pp.364-367
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• 2004

This paper presents the flight software of KoDSat (KSLV-l Demonstration Satellite) which performs demonstrating the KSLV-l (Korea Space Launch Vehicle-l)'s satellite launch capability. The KoDSat Flight Software executes in a single-processor, multi-function flight computer on the spacecraft, the OBC (On Board Computer). The flight software running on the single processor is responsible for all real-time processing associated with: processor startup and hardware initialization, task scheduling, RS422 handling function, command and data handling including uplink command and down-link telemetry, attitude determination and control, battery state of charge monitoring and control, thermal control processing.

• Journal of Astronomy and Space Sciences
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• v.21 no.2
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• pp.109-120
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• 2004

STSAT-1 was launched on sep. 2003 with the main payload of Far Ultra-violet Imaging Spectrograph(FIMS). The mission of FIMS is to observe universe and aurora. In this paper, we suggest a simple and reliable strategy adopted in STSAT-1 to synchronize time between On-board Computer(OBC) and FIMS. For the characteristics of STSAT-1, this strategy is devised to maintain reliability of satellite system and to reduce implementation cost by using minimized electronic circuits. We suggested two methods with different synchronization resolutions to cope with unexpected faults in space. The backup method with low resolution can be activated when the main has some problems.