• 한국지구물리탐사학회:학술대회논문집
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• 2008.10a
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• pp.145-148
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• 2008

ICESat launched in Jan. 2003 has a capability to monitor polar regions with its inclination of 94 degree. ICESat carries GLAS (Geosciences Laser Altimetry System) to measure Earth's topography in unprecedented accuracy, and thus it can be applied for glacier variation due to recent climate changes. Here we present a new method to estimate velocity structure of Amery Ice-Shelf using ICESat altimtery data. ICESat data shows horizontal displacement of Amery Ice-Shelf, which can be directly used for velocity estimation. This method is expected to extend to other ice-shelves in Antarctica.

• The Bulletin of The Korean Astronomical Society
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• v.37 no.2
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• pp.190.2-190.2
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• 2012

과학기술위성3호는 170kg의 소형위성으로 2006년 사업을 착수하였으며, 올 2012년 12월에 러시아에서 발사할 예정이다. 주탑재체는 다목적 적외선 영상시스템 (MIRIS, Multi-Purpose IR Imaging System)으로 천문연에서 개발을 담당하였으며 우주관측과 지구관측을 수행한다. 부탑재체는 소형영상분광기 (COMIS, Compact Imaging Spectrometer)로 공주대에서 개발을 하였으며 지표면의 분광영상을 획득한다. 관측영상을 지상에서 내려 받아 사용자에게 배포를 하기 전 Radiometric, Geometric 보정을 수행하기 위해서는 관측영상 외에 관측할 때의 위성체 자세제어 정보도 함께 필요하다. 과학기술위성3호의 경우 우주관측은 관측영상 정보에 위성본체의 자세제어 정보도 함께 저장하기 때문에 지상에서 영상자료와 관제자료의 결합을 위해 추가로 수행하는 작업이 필요하지 않다. 그러나 지구관측은 영상자료와 자세제어 정보를 따로 저장하여 지상국으로 전송한다. 한곳의 영역만 관측 후 지상국으로 전송받는다면 문제가 발생하지 않지만, 지상국과 교신할 수 있는 궤도의 수는 한정되기 때문에 위성체의 메모리에는 여러 영역의 관측영상이 저장되어 있으며, 위성은 지상국과의 교신시간이 허락하는 최대로 영상자료를 송신한다. 본 발표에서는 다양한 영상자료의 저장 포맷과 여러 영역을 관측했을 때 각 영역에 해당하는 영상자료 구분 방법, 그리고 각 영상자료와 관제자료의 결합방법에 대해 설명한다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.108-111
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• 2017

High performance upper stage engine is necessary for space launch vehicles of geostationary orbit, and staged combustion cycle engine is suitable due to high specific impulse. Technology demonstration model for 9 tonf class staged combustion cycle engine, which is consisted of turbopump, preburner, combustion chamber and supply system, was assembled, and hot-firing test was conducted for three seconds in Upper-stage Engine Test Facility of Naro Space Center. Ignition, combustion and shut down of engine system was performed normally, and its performance parameters were evaluated.

• The Bulletin of The Korean Astronomical Society
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• v.37 no.2
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• pp.157.1-157.1
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• 2012

1990년대 제안된 RTK(Real-Time Kinematics)는 GNSS/GPS 반송파 위상(carrier phase) 관측값을 이용한 방식으로 cm 수준의 정확도를 실시간으로 산출할 수 있어 측지 측량 등 다양한 분야에서 활용되고 있다. 그러나 한 가지 중요한 단점은 이 방식을 사용하는 기준국과 사용자는 10~20km 이내에 존재해야만 빠르고 신뢰할 수 있는 해를 산출할 수 있다는 점이다. 이는 궤도오차, 대류층 및 전리층 오차에 공간 상관성(spatially correlated) 있기 때문인데, 사용자 주변을 둘러싼 다중 기준국들의 측정치를 조합하여 보상하거나 모델링하여 줄이는 방식인 다중 기준국 네트워크 기반의 RTK 알고리즘이 제안되어 사용되고 있다. 다중 기준국 네트워크 기반의 RTK 프로세스에서 기준국간 미지정수 결정은 전 과정의 핵심 프로세스라고 할 수 있으며, 관련되어 많은 기술들이 제안되고 연구되어 왔다. 특히, 1980년대 말부터 현재까지 후처리 기반으로 꾸준하게 연구되고 있는 Blewitt에 의해 전리층 제거 조합과 Wide-lane 반송파 위상 조합을 활용한 미지정수 검색 방법이 대표적이며 이후에도 Gao, Colombo등 다양한 연구자에 의해 활용되었다. 이 연구에서는 실시간으로 다중 기준국 반송파 미지정수를 결정하는 기술에 대한 연구를 수행하였다. L1, L2 관측값 조합으로 인한 관측값의 잡음 수준이 증가하는 영향을 피하기 위해 L1, L2 반송파 위상 및 의사거리를 그대로 관측값으로 사용하여 사용자 위치 및 속도, 기준국간 이중 차분된 전리층 지연 수직성분, 대류층 wet 지연 수직 성분, 이중 차분된 미지정수를 미지의 상태변수로 확장 칼만필터를 통해 직접적으로 추정하는 방식으로 미지정수의 실수해를 결정하였고, 정수해는 실시간에 적합한 MLAMBDA 기법과 비율테스트를 통한 정수해 검정기법을 통해 결정하였다.

• Korean Journal of Remote Sensing
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• v.22 no.4
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• pp.255-264
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• 2006

GRACE (Gravity Recovery and Climate Experiment) is the first dedicated gravity mapping mission. Its primary measurements are the distance changes between two co-orbiting low earth satellites. GRACE is a joint development by NASA and German DLR and was launched in March 2002. GRACE improves the Earth gravity model accuracy by nearly two factor of magnitude over pre-launch models. After brief description of the GRACE primary instrument, inter-satellite ranging system, its flight status and preliminary performance evaluation is presented. Ranging system error models, which were not included in the pre-launch performance model and design specifications, are identified through analyzing the flight data. Base on this analysis, future research topics on the GRACE instrument performance analysis are discussed.

• Korean Journal of Remote Sensing
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• v.39 no.5_3
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• pp.979-995
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• 2023

As wildfires are difficult to predict, real-time monitoring is crucial for a timely response. Geostationary satellite images are very useful for active fire detection because they can monitor a vast area with high temporal resolution (e.g., 2 min). Existing satellite-based active fire detection algorithms detect thermal outliers using threshold values based on the statistical analysis of brightness temperature. However, the difficulty in establishing suitable thresholds for such threshold-based methods hinders their ability to detect fires with low intensity and achieve generalized performance. In light of these challenges, machine learning has emerged as a potential-solution. Until now, relatively simple techniques such as random forest, Vanilla convolutional neural network (CNN), and U-net have been applied for active fire detection. Therefore, this study proposed an active fire detection algorithm using state-of-the-art (SOTA) deep learning techniques using data from the Advanced Himawari Imager and evaluated it over East Asia and Australia. The SOTA model was developed by applying EfficientNet and lion optimizer, and the results were compared with the model using the Vanilla CNN structure. EfficientNet outperformed CNN with F1-scores of 0.88 and 0.83 in East Asia and Australia, respectively. The performance was better after using weighted loss, equal sampling, and image augmentation techniques to fix data imbalance issues compared to before the techniques were used, resulting in F1-scores of 0.92 in East Asia and 0.84 in Australia. It is anticipated that timely responses facilitated by the SOTA deep learning-based approach for active fire detection will effectively mitigate the damage caused by wildfires.

• Journal of the Korean Chemical Society
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• v.24 no.4
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• pp.269-279
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• 1980

A method for calulation of the magnetic moments for both octahedral and distorted octahedral $[V(III)A_3B_3]$ type complexes, all with $t^2_2$ configuration, has been developed [A and B = O, Cl, N, F or Br]. The calculated magnetic moments by this method are in reasonable agreements with the experimental values. The calculated magnetic moments for distorted octahedral $[V(III)A_3B_3]$/TEX> type complexes decrease as the extent of tetragonal distortion increases.The effects of k (orbital reduction faction factor), $\xi'$/TEX> and temperature on the magnetic moments are also investigated.A new method for calculation of the contribution of $^3T_1$ molecular orbitals to the dipole moment and polarizability has also developed. The calculated contribution of $^3T_1$ molecular orbitals falls in the reasonable range of values.

• Publications of The Korean Astronomical Society
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• v.17 no.1
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• pp.23-40
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• 2002

The spatial distribution of meteoroids or cometary debris along the orbit of the Earth is investigated by analyzing the meteoric records in the Chronicle of the Koryo dynasty (918-1392) which is called Koryosa. Sporadic meteors in this period show the seasonal variation in number, which is similar to the current meteors. We also found that there are a few spikes showing large accumulation of records around the same dates. We regard these spikes as meteor showers in the Koryo period. We compared the dates of meteor showers with those compiled from the historical records around the world including Korea, Japan, China, Arab, and European countries. We discovered three prominent showers and four weak showers. The prominent ones are the Leonids, the Perseids, and the Aquarids and the Orionids pair. The last pair is the remnants of Halley's comet. The astronomical records written in the history book of the Koryo dynasty are turned out to be accurate and written in a steady manner. We can also see that those records can be useful to contribute the development of modern astronomy and astrophysics.

• Korean journal of applied entomology
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• v.24 no.4 s.65
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• pp.231-238
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• 1986

Molecular orbital theoretical study on the stability of conformations and chemical reactivity of 0,0-diethylphenylphosphate derivatives were carried out by EHT and CNDO/2 molecular orbital calculation method. The results shown that the dipole moment(${\mu}$) and total energies of the ${\theta}=90^{\circ}$ conformer were ${\mu}=3.185D\;&\;E_t=-162.6479(au)$ and also that of the ${\theta}=0^{\circ}$ conformer were ${\mu}=5.596D\;&\;E_t=-162.4013(au)$, respectively. Therefore, the values of ${\mu}\;&\;E_t$ of the ${\theta}=90^{\circ}$ conformer were much smaller than that of the ${\theta}=0^{\circ}$ conformer. The form with angle of rotation ${\theta}=90^{\circ}$ of phenyl ring was shown to be most stable and this was interpreted in terms of electrostatic and steric effect. 0,0-diethylphenylphosphate derivatives are predicted to increase both charge and orbital controlled $SN_2$ reactivity of the electron withdrawing substituent reduces the HOMO & LUMO energy, while the electron withdrawing substituent due to increase in positive charge of phosphorus atom of phosphate molecule.

• Aerospace Engineering and Technology
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• v.12 no.1
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• pp.40-45
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• 2013

Satellite's infrared detector shall be calibrated under thermal vacuum environment using a reference black body before a launch. The full aperture black body (FABB) as an infrared calibration reference shall be composed of vacuum compatible materials and temperature controlled from $-40^{\circ}C$ to $+40^{\circ}C$ with emissivity higher than 0.95. The temperature homogeneity over the central 80 % area of the FABB front surface shall be better than 2 K. The FABB designed by thermal and flow analysis was $1m{\times}1m{\times}8mm$ copper plate on which black painted aluminum honeycomb core was attached. Copper tubes were welded on the opposite side of the honeycomb core to allow temperature regulated gaseous nitrogen to flow through them. By the FABB validation test, the temperature homogeneity was observed around 1 K using 20 PT100 sensors and modified COTS infrared camera. The emissivity value was 0.975 at $40^{\circ}C$ under atmospheric pressure.