• 한국레이저가공학회지
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• 제13권4호
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• pp.14-20
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• 2010

Robot path generation and laser welding technology for manufacturing automotive body are studied. Laser welding and industrial robot systems are used with the robot based laser welding system. The laser system used in this study is 1.6kW Fiber laser, while the robot system is 6 axes Industrial robot (payload: 130kg). The robot based laser welding system is equipped with laser scanner system for remote laser welding. The laser source, robot and laser scanner system are used to increase the processing speed and to improve the process efficiency. The welding joints of steel plate are butt and lapped joints. The quality test of the laser welding are through the observation the shape of bead on plate and cross-section of welding part. The 3 dimensional laser welding for non-linear pipe welding line is performed. This paper introduces the robot based laser welding system to resolve the limited welding speed and accuracy of the conventional spot welding system.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2007년도 추계 학술대회논문집
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• pp.227-231
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• 2007

COMS (Communication, Ocean and Meteorological Satellite) is a geostationary satellite and has been developing by KARI for communication and ocean and meteorological observations. It will be launched by ARIANE 5. Ka-band components are installed on South panel, where single solar array wing is mounted. Radiators, embedded heat pipes, external heat pipe, insulation blankets and heaters are utilized for the thermal control of the satellite. The Ka-band payload section is divided several areas based on unit operating temperature in order to optimize radiator area and maximize heat rejection capability. Other equipment for sensors and bus are installed on North panel. The ocean and meteorological sensors are installed on optical benches on the top floor to decouple thermally from the satellite. During the transfer orbit operation, satellite will be under severe thermal environments due to low dissipation of components, satellite attitudes and LAE(Liquid Apogee Engine) firing. This paper presents temperature and heater power prediction and validation of thermal control design during transfer orbit operation.

• 한국콘크리트학회:학술대회논문집
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• 한국콘크리트학회 2008년도 춘계 학술발표회 제20권1호
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• pp.93-96
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• 2008

이 논문은 근단층지반운동(NFGM)하에서 내진성능을 평가하기 위한 RC교각의 진동대, 준정적, 유사동적 실험을 다룬다. 5개의 실험체가 수행되었다. 축소 모형을 제작하고 상부구조물의 중량 에 의한 축력의 효과는 프리스트레스에 의해 구현하였다. 지진이 발생할 때 상부 구조물의 횡방향 관성력은 진동대의 제한된 용량 때문에 교각 실험체에 연결한 질량 프레임으로 모사하였다. 특히, 진동대 실험에서 질량 모사 프레임이 교각 모델과 같은 변위로 움직이면서 마찰 효과를 최소화할 수 있도록 고려하였고 이에 대한 검증을 실시하였다. RC교각의 축소 계수를 4.25로 설정 하였다.

• 한국항행학회논문지
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• 제20권1호
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• pp.8-14
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• 2016

본 논문은 한국형 위성기반보정시스템인 KASS (Korea augmentation satellite system)을 구성하는 위성통신국과 임차해 구축 예정인 2기의 정지궤도 위성이 포함된 위성통신시스템에 대한 상위개념의 설계분석 결과를 제시하였다. 위성통신국의 주요 기능인 중앙처리국으로부터의 보정정보 및 무결성 정보를 수신하여 해당 메시지에 대한 부호화, 변조 후 주파수변환 및 신호증폭에 대한 내용과 그 기능을 만족하는 설계를 위한 분석내용을 각 과정에 대한 개념, GEO 위성을 추가적인 기능인 GPS 위성 레인징 신호, GEO 레인징 신호를 사용하기 위한 GEO 위성에 대한 정밀 궤도결정기술, 그리고 GPS 위성과 GEO 위성간 시각 동기를 위한 클럭 조정에 대하여 기술하였다. 추가적으로 중계기 대역폭에 따른 GEO 위성 레인징 성능 분석결과로 SBAS 보강 서비스를 위해서는 최소한 2.2 MHz 의 GPS와 같은 레인징 서비스를 위해서는 18.5 MHz의 대역폭이 필요함을 제시하였다. 이러한 분석내용은 GEO 위성과 위성통신국의 설치장소가 최종 확정되면 최종 분석을 수행하여 KASS 위성통신시스템 설계에 반영할 예정이다.

• 대한용접접합학회:학술대회논문집
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• 대한용접접합학회 2009년 추계학술발표대회
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• pp.29-29
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• 2009

On this research, laser welding technology for manufacturing automobile body is studied. Laser welding technology is one of the important technologies used in the manufacturing of lighter, safer automotive bodies at a high level of productivity; the leading automotive manufacturers have replaced spot welding with laser welding in the process of car body assembly. Korean auto manufacturers are developing and applying the laser welding technology using a high output power Nd:YAG laser and a 6-axes industrial robot. On the other hand, the robot-based remote laser welding system was equipped with a long focal laser scanner system in robotic end effect. Laser system, robot system, and scanner system are used for realizing the high speed laser welding system. The remote laser welding system and industrial robotic system are used to consist of robot-based remote laser welding system. The robot-based remote laser welding system is flexible and able to improve laser welding speed compared with traditional welding as spot welding and laser welding. The robot-based remote laser systems used in this study were Trumpf's 4kW Nd:YAG laser (HL4006D) and IPG's 1.6kW Fiber laser (YLR-1600), while the robot systems were of ABB's IRB6400R (payload:120kg) and Hyundai Heavy Industry's HX130-02 (payload:130kg). In addition, a study of quality evaluation and monitoring technology for the remote laser welding was conducted. The welding joints of steel plate and steel plate coated with zinc were butt and lapped joints. The quality testing of the laser welding was conducted by observing the shape of the beads on the plate and the cross-section of the welded parts, analyzing the results of mechanical tension test, and monitoring the plasma intensity and temperature by using UV and IR detectors. Over the past years, Trumf's 4kW Nd:YAG laser and ABB's IRB6400R robot system was used. Nowadays, the new laser source, robot and laser scanner system are used to increase the processing speed and to improve the efficiency of processes. This paper proposes the robot-based remote laser welding system as a means of resolving the limited welding speed and accuracy of conventional laser welding systems.

• 한국전자파학회논문지
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• 제24권12호
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• pp.1128-1139
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• 2013

다목적실용위성 5호는 영상 레이더(SAR: Synthetic Aperture Radar)을 탑재하여 야간이나 구름이 있는 지역에 대해서도 지속적인 영상촬영이 가능하다. 발사 후 초기 운영 시험에서는 SAR 탑재체에 의해 관측된 영상에 대한 기하 및 복사 보정을 수행한다. 이러한 보정은 지표상의 위치 및 RCS(Radar Cross Section)을 알고 있는 보정장치에서 반사된 SAR 신호에 의해 나타난 영상 픽셀에서의 위치 및 값을 이용하여 처리된다. 이러한 보정을 위해 기존 반사기와 달리 능동 트랜스폰더는 RCS 값을 변경할 수 있으며, 내부 시간 지연 기능에 의해 가상의 위치로 이동하는 효과를 영상에서 나타낼 수 있다. 본 논문에서는 능동 트랜스폰더의 개발에 필요한 요구사항을 도출하여 이로부터 설계, 조립 및 시험결과를 정리하였다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년 영문 학술대회
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• pp.330-339
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• 2008

Ground-based interceptors(GBI) comprise a major element of the strategic defense against hostile targets like Intercontinental Ballistic Missiles(ICBM) and reentry vehicles(RV) dispersed from them. An optimum design of the subsystems is required to increase the performance and reliability of these GBI. Propulsion subsystem design and optimization is the motivation for this effort. This paper describes an effort in which an entire GBI missile system, including a multi-stage solid rocket booster, is considered simultaneously in a Genetic Algorithm(GA) performance optimization process. Single goal, constrained optimization is performed. For specified payload and miss distance, time of flight, the most important component in the optimization process is the booster, for its takeoff weight, time of flight, or a combination of the two. The GBI is assumed to be a multistage missile that uses target location data provided by two ground based RF radar sensors and two low earth orbit(LEO) IR sensors. 3Dimensional model is developed for a multistage target with a boost phase acceleration profile that depends on total mass, propellant mass and the specific impulse in the gravity field. The monostatic radar cross section (RCS) data of a three stage ICBM is used. For preliminary design, GBI is assumed to have a fixed initial position from the target launch point and zero launch delay. GBI carries the Kill Vehicle(KV) to an optimal position in space to allow it to complete the intercept. The objective is to design and optimize the propulsion system for the GBI that will fulfill mission requirements and objectives. The KV weight and volume requirements are specified in the problem definition before the optimization is computed. We have considered only continuous design variables, while considering discrete variables as input. Though the number of stages should also be one of the design variables, however, in this paper it is fixed as three. The elite solution from GA is passed on to(Sequential Quadratic Programming) SQP as near optimal guess. The SQP then performs local convergence to identify the minimum mass of the GBI. The performance of the three staged GBI is validated using a ballistic missile intercept scenario modeled in Matlab/SIMULINK.