• The Science & Technology
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• no.3 s.406
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• pp.26-31
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• 2003

컬럼비아호는 처음 만들어졌을 때 순수한 선체무게만 7만 1800kg이었으며 메일 엔진이 장착된 후에는 8만 741kg에 달했다. 전체 길이는 56.1m이며 승무원이 타는 오비터와 외부연료탱크, 고체연료 로켓 부스터 등으로 구성돼 있다. 20여 년간 27차례의 우주비행을 하면서 우주개발과 과학연구에 커다란 업적을 남긴 컬럼비아호는 지난 1월 16일 28번째 우주비행에 나섰다가 지구 착륙을 불과 10분도 남겨놓지 않은 상태에서 공중 산화했다.

• Journal of the Korean Society of Propulsion Engineers
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• v.10 no.1
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• pp.72-86
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• 2006

A technical review of current ramjet propulsion is presented. In addition to summarize the current status of ramjet technology, new key techniques like Boosting technique easily adapting total impulse of booster, flame stabilization technique with minimized ramjet combuster length, variable nozzle-inner-surface technique realizing wide flight-envelop, and thermal protection technique for long operating time are identified. Actually various Ramjet propulsion technology has been matured and expanding to both military and combined cycle application. Yet many opportunities remain to be challenged by future generations of explorers to utilize s typical ramjet propulsion system for multi-purpose(multi-platform and multi-target) missiles, for example, American JSSCM and Russian Yakhont missiles, improving both reliability of techniques and downsizing development cost of new propulsion system.

• The KSFM Journal of Fluid Machinery
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• v.3 no.2 s.7
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• pp.50-56
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• 2000

The effects of lobe shapes on the leak flow conductance of Roots-type vacuum pump are studied numerically and experimentally. The modelled lobe shape of Roots-type vacuum pump is two-lobe spur gear. The numerical analyses are performed on leak flows in Roots-type vacuum pump. It is numerically calculated using a 4th-order Runge-Kutta method and is compared with experimental results. Results show that for the case of involute lobe shape the total amount of the leak flow conductance is greater than that of cycloid and Cassini oval lobe shapes.

• Proceedings of the KIEE Conference
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• 1992.07b
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• pp.1038-1040
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• 1992

Booster is used widely as one of the step-up DC/DC power converter in power conversion process for fuel cell power plant which have the electrical characteristic of the high current density and low cell voltage. In view of control system, booster can be unstable when it is operated in broad operation range because the transfer function of booster has zero in right half plane of s-domain. So for reliable operation, controller must make the system stable in whole working range. In this paper, the two control method such as digital PID control and fuzzy control is studied for booster output voltage regulation in fuel cell plant. The design procedure of PID control and fuzzy control is described. And the experiment of designed controller action is performed in various operation points for controller performance test.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.11a
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• pp.623-626
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• 2009

Hanwha Corporation Daejeon Plant have developed apogee Kick Motor of KSLV-I that is the first among nation space launch vehicle for five years from 2003. Now, we are joining in KSLV-II(Korea Space Launch Vehicle-II) project and developing Pyro starter which is turbo pump for the first start-up of liquid propulsion supply.

• Proceedings of the KIPE Conference
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• 1998.11a
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• pp.44-48
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• 1998

In the buck-boost DC-DC converter which is used at a certain situation such as in factories where loads often change a lot, the switches in the device make big energy loss in operating at Buck-Boost Mode due to hard switching and are affected by lots of stresses which decrease the efficiency rate of the converter. In order to improve this problem, to decrease the loss of snubber and switching, it has been investigated that zero voltage switching mode and zero current switching mode which make the operation of switches with soft switching. For the more sophisticated and advanced device, this paper is presented the Partial Resonant Soft Switching Mode Power Converter which is adapted the power converter having the partial resonant soft switching mode, that makes switches operate when the resonant current or voltage becomes zero by making the resonant circuit partially at turning on and off of the switches with suitable layout of the resonant elements and switch elements in the converter. Also, this paper includes the analysis and simulation of the Partial Resonant type Buck-Boost Chopper.

• Journal of Institute of Control, Robotics and Systems
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• v.18 no.6
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• pp.519-525
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• 2012

Electric brake booster systems replace conventional pneumatic brake boosters with electric motors and rotary-todisplacement mechanisms including ECU (Electronic Control Unit). Electric booster brake systems require precise target pressure tracking and control robustness because vehicle brake systems operate properly given the large range of loading and temperature, actuator saturation, load-dependent friction. Also for the implement of imbedded control system, the controller should be selected considering the limited memory size and the cycle time problem of real brake ECU. In this study, based on these requirements, a sliding mode controller has been chosen and applied considering both model uncertainty and external disturbance. A mathematical model for the electric booster is derived and simulated. The developed sliding mode controller considering chattering problem has been compared with a conventional cascade PID controller. The effectiveness of the controller is demonstrated in some braking cases.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1999.10a
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• pp.28-28
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• 1999

본 연구에서는 가스 발생기에서 발생되는 고온, 고압의 가스를 이용하여 유도탄을 수직 발사하는 사출 시스템에 대해 해석적 연구를 수행하였다. 사출 시스템에 의한 수직발사 방식은 발사관내에 설치된 가스 발생기에 의해 생성된 가스가 사출 실린더의 피스톤을 구동시켜, 피스톤에 연결된 유도탄을 요구되는 높이로 사출 시킨 후 유도탄이 점화되는 발사방식이다. 이러한 발사방식은 유도탄 자체의 부스터 발사방식에 비해 유도탄의 화염에 의한 영향이 적다. 현재 사출 시스템은 가스발생기, 가스 튜브, 사출 실린더와 피스톤으로 구성되어있다. 본 논문은 가스 발생기에서 사출 실린더까지의 내부 유동장을 일차원적으로 모델링하였고, 가스발생기, 가스튜브, 실런더 내의 유동과 열전달 과정 및 유도탄의 동적거동에 대한 미분방정식을 연립하여 4th-order Runge-Kutta 방법으로 계산하였다. 또한 가스튜브와 사출 실린더의 열전달 손실에 대하여 1차원 비정상 열전도 방정식의 수치적 계산을 통해 에너지 손실을 계산하였다. 특히 해석에 사용된 작동유체인 추진제 가스의 열학적 상태량은 온도 함수의 5차 다항식으로 표현하여 사용하였다. 이론적인 해석을 통해 사출 장치 시스템의 성능 요구조건과 신뢰성을 만족시키기 위한 가스발생기의 추진제 그레인 및 사출 시스템 설 계 조건을 도출하였다.

• Journal of the Korean Institute of Telematics and Electronics S
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• v.34S no.9
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• pp.118-125
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• 1997

This paper proposed a new partial resonant 3.PHI. AC-DC boost converter of high efficiency using lossless snubber. The proposed converter, DCM (Discontinuous Current Mode) has a merit of simple controlled circuit because the input current control discontinuously. But turned off switching loss and stress of the switching device increase when the switch turned off at the peak of current. Therefore, the paper improves efficiency by adopting the PRS$^{2}$(Partial Resonant Soft Switching) in 3.PHI. AC-DC boost converter and makes the unity power factor. The PRS$^{2}$ is reduced a current/voltage stresses of switching devices. Also, a DCMPRS$^{2}$M(Discontinuous Conduction Mode Partial Resonant Soft Switching Method) appear the current and voltage equation of this circuit. The paepr examine in a 3.PHI. AC-DC boost converter and show the result of that.

• Proceedings of the KIEE Conference
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• 2008.07a
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• pp.1075-1076
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• 2008

이 논문에서는 전류형 MPPT(Maximum Power Point Tracking) 기법을 제안하고 적용하여 태양광 PCS(Power Conditioning System)의 기본적인 제어기를 설계하고 구현하였다. 기본적인 무변압기형 토폴로지에 전류 MPPT를 수행하고 이때에 얻어진 기준전류를 dc/dc 부스트 컨버터를 통해 dc-link에 전압을 충전하여 준다. 이 충전된 파워는 인버터를 통해 계통에 공급되게 된다. 이처럼 크게 MPPT제어, dc/dc컨트롤러, dc-link전류제어, 인버터 전류제어로 나뉘며 본 논문에서는 각 부분의 제어기를 살펴보고 실험을 통해 제어기의 성능을 확인하였다. 실험결과 제안된 전류 MPPT는 원활히 파워를 공급해주었고 dc/dc 부스터 컨버터를 거처 인버터 단까지 파워를 안정적으로 발전하는 것을 확인하였다.