• 항공우주기술
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• 제1권1호
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• pp.72-83
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• 2002

본 논문은 다목적실용위성 전력시스템의 초기 설계과정으로, 2000년 11월 ASTRIUM과 KARI에서 진행한 다목적실용위성 2호기 전력시스템의 용량설계와 태양전지 어레이의 설계를 기술하였다. ASTRIUM은 다목적실용위성 2호기 전력시스템의 기본설계를 위하여, ASTRIUM의 기존 위성 프로그램인 CHAMP 위성과 GlobalStar 위성에 적용한 전력설계 개념을 고려하였다. 그러나 전력시스템의 설계는 전력운용 개념, 각 전장품 및 전력원의 특성에 따라 설계가 다르다. 그리고 ASTRIUM사의 전력시스템 운용개념은 다목적실용위성 1호기와 다르며, 전력시스템에 사용한 전력원과 각 전장품의 상이한 특성으로 전력시스템의 설계에 근본적인 차이가 있음을 미리 밝혀둔다. 따라서 본 논문은 2호기의 제안서에 기술된 내용을 중심으로 ASTRIUM과 KARI에서 수행한 2호기 전력시스템의 기본설계를 요약하였다.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2003년도 하계학술대회 논문집 B
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• pp.985-987
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• 2003

This paper presents a design and characteristics analysis of a SRM drive for EPS application. A rack mounted EPS system is considered in this paper. A conventional driving room space and mechanical structure are suggested in design stage. In the restricted design conditions, motor parameters are determined for sufficient torque and speed. For the smooth torque generation and simple circuit of power system, 12/8 motor drive is considered. With FEM and magnetic circuit analysis, designed motor is simulated to meet the requirement of specifications. Effectiveness of the suggested SRM drive for EPS application is verified by the manufactured prototype motor drive tests.

• 항공우주기술
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• 제1권2호
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• pp.57-65
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• 2002

위성의 전력시스템은 임무기간 동안, 성공적인 임무수행을 위하여 위성의 탑재체와 위성버스에 충분한 전력을 공급하여야 한다. 전력시스템의 설계는 위성이 임무를 수행할 우주환경, 임무기간, 임무특성, 그리고 할당된 예산 등에 따라 설계의 방향이 결정된다. 즉, 1차 전력원으로 사용할 태양전지의 선정, 2차 전력원인 배터리의 선정, 그리고 각 전장품의 사양이 임무특성과 예산에 따라 결정된다. 위성의 전력시스템 설계는 다른 시스템의 설계에 큰 영향을 미칠 수 있다. 보다 많은 전력을 공급하기 위하여, 일차 및 이차 전력원을 크게 설계하는 것은 바람직하지 못하다. 위성의 필요한 전력보다 크게 설계된 전력시스템은 1차 및 2차 전력원의 잉여전력에 따른 열 발생문제, 임무수행에 따른 자세제어 문제, 각 전장품의 전력 용량 문제, 그리고 발사체의 선정 및 발사비용 등의 문제를 일으킨다. 특히, 저궤도의 경우에는 orbit drag 현상에 따른 위성의 궤도 유지보수를 위하여 추진제의 용량설계에 큰 영향을 줄 수 있다. 따라서, 전력시스템의 최적설계와 효율적인 운용을 위한 여러 기술이 개발되고 있다.

• 산업공학
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• 제13권2호
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• pp.157-165
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• 2000

In this paper, an efficient method is proposed to place the cooling lines(CLS) and ejector pins(EPS) of mold design. The other components of mold, except CLS and EPS, can be generated automatically by batch processing. But the placements and sizes of CLS and EPS depend on the shapes of a part, so that the design works of CLS and EPS should be processed interactively. Using the pre-defined reference points, the positions of CLS and EPS can be determined interactively. By the proposed method, the interference occurred during placing CLS and EPS can be avoided, and the proper lengths of them can be calculated automatically. The information of the positions and lengths are stored in BOM database for generating a machining data. The proposed method is implemented with Unigraphics API functions and C language, tested on Unigraphics V15.

• Journal of Power Electronics
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• 제6권1호
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• pp.18-28
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• 2006

The Electric Power Subsystem (EPS) is one of the most critical systems on any satellite because nearly every subsystem requires power. This makes the choice of power systems the most important task facing satellite designers. The main purpose of the Satellite EPS is to provide continuous, regulated and conditioned power to all the satellite subsystems. It has to withstand radiation, thermal cycling and vacuums in hostile space environments, as well as subsystem degradation over time. The EPS power characteristics are determined by both the parameters of the system itself and by the satellite orbit. After satellite separation from the launch vehicle (LV) to its orbit, in almost all situations, the satellite subsystems (attitude determination and control, communication and onboard computer and data handling (OBC&DH)), take their needed power from a storage battery (SB) and solar arrays (SA) besides the consumed power in the EPS management device. At this point (separation point, detumbling mode), the satellite's angular motion is high and the orientation of the solar arrays, with respect to the Sun, will change in a non-uniform way, so the amount of power generated by the solar arrays will be affected. The objective of this research is to select satellite EPS component types, to estimate solar array illumination parameters and to determine the efficiency of solar arrays during both detumbling and normal operation modes.

• 전력전자학회:학술대회논문집
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• 전력전자학회 2003년도 추계학술대회 논문집
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• pp.190-192
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• 2003

This paper presents a design and characteristics analysis of an SRM drive for EPS application. A rack mounted EPS system is considered in this paper. In the unrestricted design conditions, motor parameters are determined for sufficient torque and speed. For the smooth torque generation and simple circuit of power system, 12/8 motor drive is considered. With FEM and magnetic circuit analysis, redesigned motor is simulated to meet the requirement of specifications. Effectiveness of the suggested SRM drive for EPS application is verified by redesigned motor drive tests.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2003년도 춘계학술대회 논문집 전기기기 및 에너지변환시스템부문
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• pp.13-15
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• 2003

This paper presents a design and characteristics analysis of a SRM drive for EPS application. A rack mounted EFS system is considered in this paper. A conventional driving room space and mechanical structure are suggested in design stage. In the restricted design conditions, motor parameters are determined for sufficient torque and speed. For the smooth torque generation and simple circuit of power system, 12/8 motor drive is considered. With FEM and magnetic circuit analysis designed motor is simulated to meet the requirement of specifications. Effectiveness of the suggested SRM drive for EPS application is verified by the manufactured prototype motor drive tests.

• 전력전자학회:학술대회논문집
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• 전력전자학회 2003년도 춘계전력전자학술대회 논문집(2)
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• pp.836-839
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• 2003

This paper presents a design and characteristics analysis of a SRM drive for EPS application. A conventional driving room space and mechanical structure are suggested in design stage. In the restricted design conditions, motor parameters are determined for sufficient torque and speed. For the smooth torque generation and simple circuit of power system, 12/8 motor drive is considered. With FEM and magnetic circuit analysis, designed motor is simulated to meet the requirement of specifications. Effectiveness of the suggested SRM drive for EPS application is verified by the manufactured prototype motor drive tests.

• 조명전기설비학회논문지
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• 제24권8호
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• pp.27-31
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• 2010

EPS(Elctrical Power Steering)에서 전동기의 토크 리플은 조향장치의 진동 문제를 야기한다. 따라서 EPS에서 전동기의 토크 리플 저감은 중요한 문제이며, 본 논문에서는 EPS에서 사용하는 표면부착형 영구자석 동기전동기의 토크 리플 저감에 대해 논하였다. 유한요소법을 이용하여 영구자석과 고정자 슈의 형상 변화를 통해 역기전력을 분석하였으며 이를 바탕으로 토크 리플 저감 방안을 제시하였다.

• 한국정밀공학회지
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• 제29권12호
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• pp.1351-1359
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• 2012

Due to the development of electric and hybrid vehicles, the trend has changed from hydraulic power steering system to electric power steering system (EPS). In this paper, design parameters are deduced through the structural analysis based on the finite element analysis for the intermediate shaft of the EPS on the market. By analyzing the design parameters, the structure design is improved to support the required high torque on the EPS. The numerical analysis is performed to obtain the improved design of the intermediate shaft model and the analysis results are compared with the existing model. It is noted through this numerical approach that the improved design of the intermediate shaft can be acquired the structural safety and high stiffness than existing model.