• 조명전기설비학회논문지
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• 제28권11호
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• pp.17-25
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• 2014

This paper proposes a novel maximum power point tracking (MPPT) system using a fuzzy logic control (FLC) algorithm for robust in-environment changing. The power available at the output of a photovoltaic (PV) cell continues to change with radiation and temperature because a solar cell exhibits nonlinear current-voltage characteristics. Therefore, the maximum power point (MPP) of PV cells varies with radiation and temperature. The MPPT methods are used in PV systems to make full utilization of the PV array output power, which depends on radiation and temperature. The conventional MPPT control methods such as constant voltage (CV), perturbation and observation (PO) and incremental conductance (IC) have been studied but these methods are problematic in that they fail to take into account the changing environment. The proposed FLC controller is based on the fuzzy control algorithm and facilitates robust control with the environmental changes. Also, the PV systems applied FLC controller is modeled by PSIM and the response characteristics of the FLC method according to environmental variations are analyzed through comparison with the performance of conventional methods. The validity of this controller is shown through response results.

• 한국전기전자재료학회:학술대회논문집
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• 한국전기전자재료학회 2008년도 하계학술대회 논문집 Vol.9
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• pp.377-378
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• 2008

Space charge formation in various glass materials under electron beam irradiation was investigated. Charging of spacecraft occurs in plasma and radiation environment. Especially, we focused on an accident caused by internal charging in a glass material that was used as the cover plate of solar panel array, and tried to measure the charge distribution in glass materials under electron beam irradiation by using a PEA (Pulsed Electro-Acoustic method) system. In the case of a quartz glass (pure $SiO_2$), no charge accumulation was observed either during or after the electron beam irradiation. On the contrary, positive charge accumulation was observed in glass samples containing metal-oxide components. It is found that the polarity of the observed charges depends on the contents of the impurities. To identify which impurity dominates the polarity of the accumulated charge, we measured charge distributions in several glass materials containing various metal-oxide components and calculated the trap energy depths from the charge decay characteristics of all glass samples. Furthermore, the dependence of the polarity of accumulated charges on the component of glass materials is discussed by using the models of energy bands.

• 대한기계학회논문집A
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• 제26권4호
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• pp.602-608
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• 2002

The flexible structure like solar array and antenna in spacecraft shows very sensitive responses to the inner or outer disturbance and noise. And the spacecraft becomes more complex and larger as it has various mission and role. But since the spacecraft need to have the limited mass, the thin and light material should be selected and this necessity induces the decrease d natural frequency and structural stiffness. It reduces the ability of adapting to the disturbance and induces the structural unstability. Certainly, the disturbance does not only make the structural unstability, but also give the bad effect to the precise attitude control. So it is necessary to control the vibration in the space. In this paper, the flexible structure control modeling with piezo sensor and piezo actuator is developed. The model uncertainty of damping ratio is overcome by robust control. The system equation is induced by the finite element method.

• 천문학논총
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• 제30권2호
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• pp.761-763
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• 2015

Colors have been derived from the observed optical spectrum of Mars and Jupiter. It is known that the planets and the Moon emit reflected sunlight and thus their spectra are similar to the spectrum of solar radiation. The question was then why is the color of Mars different from that of other planets, i.e. red, although it would share the same spectrum of reflected sunlight. Can one derive color from the spectrum? Therefore, we observed the optical spectra of the scattered sunlight in day time for the Moon and Mars using a 1-D array spectrograph on the 12-inch reflecting telescope in the Korea Science Academy of KAIST in Busan, Korea. We adopted the International Commission on Illumination (CIE) in 1931 of three spectral sensitivity peaks for the human eye in short, medium and long wavelengths in visible light. The observed spectra were imposed on CIE sensitivities and the color detected by the human eye was derived. The Mars spectrum represents red color and the Moon white. It is a similar color to that which a human would see. This result means that color is easily derived from astronomical spectra. The appearance of the planets surface can be determined for Mars, which is the result of iron oxide.

• 한국조명전기설비학회:학술대회논문집
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• 한국조명전기설비학회 2004년도 춘계학술대회 논문집
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• pp.442-446
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• 2004

KOMPSAT series use software-controlled unregulated bus system in which the main bus is directly connected to a battery and the duty-ratio for PWM switch is controlled by the on-board satellite software. This paper proposes a new power-stage circuit that can be available for modularization of the power regulator which is used at the software-controlled unregulated bus system satellite. And we analyze the proposed power-stage operation according to its operating modes and verify it by performing software simulation and hardware experiment using prototype. We constructs a parallel-module converter which is composed of proposed power-stages and perform experiment to verify modular characteristics of the proposed power-stage. Finally, we verify the usefulness of the proposed power-stage by comparing above results with those of a parallel-module converter made of conventional power-stages.

• 한국위성정보통신학회논문지
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• 제5권1호
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• pp.69-74
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• 2010

통신해양기상위성 개발 과정의 일환으로 통신해양기상위성이 아리안-5ECA 발사체에 탑재되어 발사될 때 발생되는 음향하중으로 부터 안전한가를 검증하기 위하여 음향진동 시험이 수행되었다. 본 논문에서는 통신해양기상위성개발 과정에서 수행된 음향진동시험과 관련하여 시험 준비 과정을 설명하고, 시험 결과에 대한 검토를 통하여 통신해양기상위성이 발사 시 경험하게 되는 음향하중에 대하여 안전한지 검토하였다. 태양전지판, Ka Band 통신탑재체 안테나 및 피드, 해양탑재체, 기상탑재체 등에 대한 상세한 검토를 통하여 통신해양기상위성이 발사 시 음향하중으로부터 안전하다는 것을 확인하였다.

• 항공우주시스템공학회지
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• 제15권4호
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• pp.57-63
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• 2021

The launch vehicle (LV) separation detection interface of the satellite, which is designed to initiate the launch and early operation phase (LEOP) for S-band data transmission and the solar array deployment after the LV separation, is one of the hazard items at the launch site. Therefore, this interface should satisfy the single-fault tolerance requirement for the range safety. In this paper, we discuss the LV separation detection interfaces for two different satellite launch configurations and propose a method to guarantee for the satellite to start the LEOP even under the emergency case such as a partial separation from the LV. Furthermore, the proposed method meets the range safety requirement of the launch site. As this method only changes the external harness configuration of the satellite, it increases the reliability of the satellite early operation without any modification of the existing internal logics to detect the separation event.

• International Journal of Computer Science & Network Security
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• 제22권3호
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• pp.355-363
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• 2022

This paper presents the modeling for islanded hybrid AC/DC microgrid and the verification of the proposed supervisory controller for energy management for this microgrid. The supervisory controller allows the microgrid system to operate in different power flows through the proposed control algorithm, it has several roles in the management of the energy flow between the different components of the microgrid for reliable operation. The proposed microgrid has both essential objectives such as the maximum use of renewable energies resources and the reduction of multiple conversion processes in an individual AC or DC microgrids. The microgrid system considered for this study has a solar photovoltaic (PV), a wind turbine (WT), a battery (BT), and a AC/DC loads. A small islanded hybrid AC/DC microgrid has been modeled and simulated using the MATLAB-Simulink. The simulation results show that the system can maintain stable operation under the proposed supervisory controller when the microgrid is switched from one operating mode of energy flow to another.

• 공업화학
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• 제24권5호
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• pp.443-455
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• 2013

혼합되지 않는 두 용액 사이의 계면(interface between two immiscible electrolyte solutions, ITIES)에서의 전하 이동 반응에 대한 전기화학적 연구는 이온 검출용 센서, 바이오센서, 생체막 모델링, 약물 전달 반응, 상전이 촉매반응, 연료 생성, 태양에너지 전환 등을 포함한 다양한 연구 분야에 적용이 가능하기 때문에 크게 주목받고 있다. 특히 ITIES에서의 이온 전이 반응을 이용하여 이온물질 및 생물질 등을 검출할 수 있는 센서로 개발하기 위해 불안정한 ITIES의 한 쪽 액체층을 젤(gel)화하여 안정화하고, 마이크로 계면 형성을 통해 전압강하를 최소화 시키는 등의 연구가 활발하게 이루어졌다. 본 총설에서는 ITIES 계면에서의 이온 전이 반응을 이용하여 개발된 다양한 센서의 원리와 응용 및 발전 가능성에 대해 다루고자 한다. ITIES 계면을 (i) 보편적인 액체/액체 계면형, (ii) 마이크로피펫 팁형, (iii) 고분자 박막에 형성된 단일 마이크로홀 또는 마이크로홀 어래이형 및 (iv) 실리콘 기판에 제작된 마이크로홀 어래이형으로 분류하고, 이들 계면에서의 직접적인 이온 전이 반응과 보조 이온 전이 반응을 활용하여 수질 환경 오염의 원인이 되는 이온 및 농약 성분을 선택적으로 검출할 수 있는 이온 선택성 센서와 생물질을 분석할 수 있는 바이오센서 개발 연구에 대해 초점을 두고 소개하려 한다.

• Journal of Astronomy and Space Sciences
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• 제14권2호
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• pp.275-285
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• 1997

1989년 2월에 일본의 우주과학연구소(ISAS: Institute of Space and Astronautical Science)에서 발사한 과학위성 EXOS-D의 전기장 측정기와 지자기 자오선 동경 190/210 선상에 위치하고 있는 17개의 지상자력계들로부터 1994년 11월 09일 18시 50분부터 약 20분에 걸쳐 Pi 2 파동이 검출되었다. 우리가 이용한 지상자력계는 지자기 경도는 동경 185.02에서 동경 269.36사이, 지자기 위도는 -37.09에서 65.67사이에, L값은 1.00에서 5.89사이에 위치하고 있다. 또한 같은 시각에 또 다른 위성 ETS-VI의 자기장 측정기의 자료와 지상의 Kakioka(지자기 동경 208.00, 지자기 위도 26.70), Hermanus(지자기 동경 82.97, 지자기 위도 -33.78) 지상자력계의 자료도 함께 사용하여 비교하여 보았다. Pi 2 파동의 주파수를 알아내기 위하여 FFT를 이용하였으며, L값이 2.35인 EXOS-D 위성과 지상자력계들에서는 주파수가 약 25mHz에서 최대 값을 보였으나, L값이 6.60인 ETS-VI위성에서는 같은 주파수가 검출되지 않았다. 또한 지상자력계 중에서 MUT 지상자력계의 자료를 기준으로 하여 위성들과 나머지 지상자력계들간의 상관관계, 위상 차를 조사하여, 발견된 Pi 2 파 동 현상이 플라즈마구 내에서 형성된 공동(cavity) mode에 의한 현상임을 알 수 있었다.