• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2005.11a
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• pp.426-430
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• 2005

The COMS(Communication, Ocean and Meteorological Satellite) is the first developed three-axis stabilization multi-function satellite on geostationary earth orbit(GEO) in korea, presently scheduled to be launched in 2008. The COMS propulsion system provides the thrust and torque required for the insertion into GEO, attitude and orbit control/adjustment of spacecraft. In this paper, system design of propulsion system, basic functions and design requirement of components are described.

• Proceedings of the KIEE Conference
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• 2006.07b
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• pp.1107-1108
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• 2006

본 논문에서는 교통 분야의 새로운 미래 성장동력분야 창출로 Global Standard도출하여 세계시장 선점 및 진출하자는 거대한 목표에 따라 IT기반의 네트워크 운행제어 시스템을 바탕으로 차량, 전력, 분기, 선로구축물 등의 하부시스템의 각종방식을 비교 및 검토하여 열차 시스템에 부합되게 선정하는 시스템설계를 수행하였다. 본 소형궤도열차시스템은 전세계적으로 영업운행 중인 노선이 없고, 운영 및 설계개념, 시스템 구성 등도 나라마다 상이하여 시스템의 개념정립을 통한 개발목표 사양(안)을 결정하는데 크게 참고가 될 만한 해외시스템이 많지 않은 실정이다. 따라서 본 연구에서는 이와 같이 제한된 참고자료와 경량전철시스템 기술개발사업에서 축적된 시스템엔지니어링 기술을 활용하여 첨단성, 친환경성, 경제성을 갖춘 소형궤도열차 시스템의 설계를 수행하였고 시스템을 구성하는 하부시스템을 정의하였다.

• Proceedings of the KIEE Conference
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• 2005.07c
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• pp.2360-2362
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• 2005

전기철도 분야에서 전자기파에 의한 환경영향 평가는 중요한 요소가 되고 있으며 급전시스템, 신호시스템, 차량시스템 등으로 나누어 각각에 대한 전자기파 환경 영향에 대한 평가에 관한 사항이 연구 중에 있다. 특히 신호시스템 중, AF(Audio Frequency)궤도회로는 철도차량과의 빈번한 통신을 통하여 철도차량 제어에 많은 역할을 담당하므로 잡음에 취약하고 오동작은 사고로 직결되므로 이러한 잡음에 대한 평가는 중요하다 할 수 있다. 본 논문에서는 전기철도차량과 신호시스템 중 AF궤도회로와의 전자기적합성을 입증할 수 있는 고조파 분석을 통한 전도성잡음의 시험 및 평가에 대한 방안을 제시한다.

• Magazine of the Korea Concrete Institute
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• v.26 no.1
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• pp.41-45
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• 2014

• The Bulletin of The Korean Astronomical Society
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• v.34 no.1
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• pp.165.1-165.1
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• 2009

• Journal of Institute of Control, Robotics and Systems
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• v.3 no.1
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• pp.61-66
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• 1997

로보트 매니퓰레이터가 일정한 접촉 힘을 유지하며 공작물의 표면을 따라가게 하는 작업은 많은 자동화 생산공정에서 유용하게 이용될 수 있다. 일반적인 위치제어용 산업용 로보트를 이러한 공정에 사용하기 위해서는 접촉힘이 계측되어 로보트의 제어에 이용되어야만 한다. 이 연구는 accommodation force control 방식으로 산업용 로보트를 제어하여 edge-following에 응용하도록하며, 접촉 힘의 계측에는 wrist force sensor를 사용한다. 이 시스템의 궤도추적속도와 force regulation 등이 예견제어에 의해 향상될 수 있다. 예견제어에 의해 설계된 전체 제어 시스템은 feedback 제어기와 feedforward 예견제어기로 구성된다. 여기서, 시스템의 안정성은 feedback 제어기에 의해서 결정되며, 예견제어기는 시스템에 미치는 외란을 통제하는 것을 주 기능으로 한다. 일반적으로 선형제어 방식을 채택한 경우와 예견제어를 이용한 edge-following을 실험을 통해 비교함으로써, 예견제어의 효용성을 확인한다.

• Proceedings of the Korean Society of Machine Tool Engineers Conference
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• 2002.04a
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• pp.76-81
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• 2002

The characteristics of the track are important concerning the mobility of tracked vehicles. It can be represented in terms of the track tension and maintaining the track tension adequately guarantees the stable and improved driving of the tracked vehicles. The track tension must be known in order to be controlled and it needs to be estimated in real-time because it is difficult to be measured. The tension around idler and sprocket can be controlled by the frizzy logic control system base on the estimated values. Dynamic Track Tensioning System(DTTS) which is estimating and controlling the track tension. In this paper, simulation tool is developed in order to apply the DTTS to real battle tanks. To construct the simulation tool, the Modeling the tracked vehicle, constructing estimation system, and designing controller should be achieved first and then all subsystem should be organized in one. The simulation tool make the RecurDyn model of tracked vehicle, which is plant model, and the control system exchange their data simultaneously. Simulation with many kinds of driving conditions and road conditions is carried out and the results are interpreted. The interpretation provides necessary information to apply the DTTS to real battle tanks.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.25 no.10
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• pp.1678-1683
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• 2001

The mobility of tracked vehicles is mainly influenced by the interaction between tracks and soil, so that the characteristics of their interactions are quite important fur the tracked vehicle study. In particular, the track tension is closely related to the maneuverability of tracked vehicles and the durability of tracks and suspension systems. In order to minimize the excessive load on the tracks and to prevent the peal-off of tracks from the road-wheels, the Dynamic Track Tensioning System (DTTS) which maintains the optimum track tension throughout the maneuver is required. It consists of track tension monitoring system, track tension controller and hydraulic system. In this paper, a dynamic track tensioning system is developed for tracked vehicles which are subject to various maneuvering tasks. The track tension is estimated based on the idler assembly model. Using the monitored track tension and con sidering the highly nonlinear hydraulic units, fuzzy logic controllers are designed in order to control the track tension. The track tensioning performance of the proposed DTTS is verified through the simulation of the Multi -body Dynamics tool.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.11a
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• pp.807-808
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• 2010

To insert payload to the orbit over the 200km-altitude using launch vehicle which has 300sec the Isp, multi staging technique for launch is necessary. The range between the sea-level to the transfer orbit about 200~250km is for operation of 1st and 2nd rocket engines and the higher altitude is for propulsion system of the acceleration block and satellite. The upper stage rocket engine should have the high technology for entering the payload into the orbit precisely more than the performance for high thrust level. With this investigation of the upper stage rocket engines which have been used, we want to understand their development trend and prospect which is going to be references for the development of ours.

• Journal of the Korean Society of Propulsion Engineers
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• v.3 no.4
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• pp.1-11
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• 1999

Thermal behavior of spacecraft propulsion system utilizing monopropellant hydrazine ($N_2$$H_4$) is addressed in this paper. Thermal control performance to prevent propellant freezing in spacecraft-operational orbit was test-verified under simulated on-orbit environment. The on-orbit environment was thermally achieved in space-simulation chamber and by the absorbed-heat flux method that implements an artificial heating through to the spacecraft bus panels enclosing the propulsion system. Test results obtained in terms of temperature history of propulsion components are presented and reduced into duty cycles of the avionics heaters which are dedicated to thermal control of those components. The duty cycles are subsequently converted into the electrical power required in the operational orbit. Additionally, cyclic temperature of each component, which was made under thermal-balanced condition of spacecraft, is compared to the acceptable design range and justified from the viewpoint of system verification.