• 한국항공우주학회지
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• 제44권4호
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• pp.352-362
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• 2016

본 논문에서는 저궤도 위성의 한 예제로써 우주파편 완화 가이드라인을 준수하는 아리랑 2호 위성의 폐기기동에 대한 분석을 수행하였다. 분석은 상용소프트웨어인 STK$^{(R)}$와 ESA의 우주파편 분석 툴 DRAMA를 사용하였으며, 가이드라인 규정 중 '25년 규정'을 만족하는 적정 폐기고도를 산출하였고, 아리랑 2호 위성의 비제어 재진입을 가정하여 내부부품의 생존률 및 지상피해면적을 분석하였다. 마지막으로 비제어 재진입 시 내부부품의 생존을 가정했을 때 다양한 초기궤도 오차를 수렴할 수 있는 적정 재진입 초기궤도를 분석하였다. 분석결과 아리랑 2호 위성은 '25년 규정' 만족을 위해 최소 43km에서 최대 105km의 고도하강이 필요하며, 비제어 재진입 시 질량이 큰 물체나 내열성이 강한 부품이 생존하여 $4.3141m^2$의 피해면적을 야기하였다. 마지막으로 재진입 초기궤도의 승교점경도를 129도로 설정했을 때 일정수준의 오차를 포함하더라도 가이드라인 기준을 만족하는 인명 피해확률을 보여주었다.

• 대한원격탐사학회지
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• 제24권4호
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• pp.351-358
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• 2008

2010년 발사 예정인 다목적실용위성 5호 (KOMPSAT-5, KOrea Multi-Purpose SATellite-5)는 기상상태와 태양고도에 제약을 받지 않고 영상 획득이 가능한 SAR(Synthetic Aperture Radar) 시스템이 탑재된다. 본 연구에서는 SAR를 이용한 레이더 측량기법 (radargrarnrnetry)을 적용하기 위하여 KOMFSAT-5의 예상 궤도와 영상 모드를 분석하여 최적의 영상 조합을 제시하였다. 임의의 지상점에서 가장 가까운 위치에 있는 궤도로부터 패스번호를 부여하였고, 충분한 고도해상도를 얻기 위해 시차(parallax)에 따른 도민감도는 0.5이상을 선택하였으며, 레이더 영상의 기하왜곡을 고려하여 고도민감도가 0.8이하가 되는 영상 조합을 최적 조건으로 제시하였다. 예를 들어, 인접한 패스간의 거리가 약 95 km인 적도에서는 기하학적 모델을 이용하여 패스번호 3-9와 5-3의 두 쌍이 최적의 영상조합으로 제시되었다. 또한 임의로 선택한 대전과 남극 세종기지 지점에서는 STK 소프트웨어를 통해 궤도를 계산하였다. 대전에서는 5-4, 7-5, 8-5의 세 영상 조합을, 남극 세종기지에서는 8-6, 9-7, 10-7, 11-8, 12-8, 13-9, 14-9, 15-9, 15-10, 15-11의 열 쌍의 영상 조합이 레이더 측량기 법에 최적임을 제시하였다.

• 한국터널지하공간학회 논문집
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• 제21권4호
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• pp.455-478
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• 2019

본 논문에서는 고강도 강관을 이용한 강관 보강 그라우팅의 보강 효과 검증을 통해 현장 적용성에 관한 실험적 내용을 다루었다. 기존 강관보강 그라우팅 공법에는 SGT275 (구 STK400) 강관을 일반적으로 적용하고 있으나, 강관 보강 그라우팅이 적용된 터널의 붕락사례를 보면 강관의 과도한 꺾임, 파단 등의 사례가 발생되고 있다. 이러한 사례가 발생하는 여러 원인 중 굴착에 따른 터널의 이완하중에 대응하는 강관의 강성 부족이 그 원인이 될 수 있다. 최근 들어 고강도 강관(SGT550)의 개발로 강관의 강도가 증가했으나, 강도 증대를 고려한 보강방안에 대한 연구가 미흡하므로 이에 대한 연구가 필요한 실정이다. 따라서 본 연구에서는 고강도 강관과 일반 강관의 이음 유무, 주입재의 충전 여부 등 다양한 조건에 대해 인장강도 및 휨 전단력 실험을 수행하고, 기존 제시된 설계법을 통해 강관의 강도 차이에 따른 효율적인 현장 적용성에 대한 기초 연구를 수행하였다. 특히, 실제 현장에 고강도 강관과 일반 강관을 시공하고 굴착에 따른 강관의 변위형상과 응력에 대한 계측 결과를 통해 고강도 강관의 보강 효과를 검증하였다. 연구결과 고강도 강관은 휨 강도가 우수하여 보강효과가 우수한 것으로 나타났으며, 강도 증진효과로 인해 아칭효과도 기대된다.

• Journal of Astronomy and Space Sciences
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• 제37권2호
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• pp.117-129
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• 2020

In a Satellite communication system, a link budget analysis is the detailed investigation of signal gains and losses moving through a channel from a sender to receiver. It inspects the fading of passed on data signal waves due to the process of spreading or propagation, including transmitter and receiver antenna gains, feeder cables, and related losses. The extent of the proposed tool is to make an effective, efficient, and user-friendly approach to calculate link budget analysis. It is also related to the satellite communication correlation framework by building up a graphical interface link analysis tool utilizing STK^® software with the interface of C# programming. It provides better kinds of graphical display techniques, exporting and importing data files, printing link information, access data, azimuth-elevation-range (AER), and simulation is also possible at once. The components of the link budget analysis tool include transmitter gain, effective isotropic radiated power (EIRP), free space loss, propagation loss, frequency Doppler shift, flux density, link margin, elevation plot, etc. This tool can be useful for amateur users (e.g., CubeSat developers in the universities) or nanosat developers who may not know about the RF communication system of the satellite and the orbital mechanics (e.g., orbit propagators) principle used in the satellite link analysis.

• Asian Pacific Journal of Cancer Prevention
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• 제14권6호
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• pp.3403-3409
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• 2013

Breast cancer is the most common cancer among women affecting up to one third of tehm during their lifespans. Increased expression of some genes due to polymorphisms increases the risk of breast cancer incidence. Since mutations that are recognized to increase breast cancer risk within families are quite rare, identification of these SNPs is very important. The most important loci which include mutations are; BRCA1, BRCA2, PTEN, ATM, TP53, CHEK2, PPM1D, CDH1, MLH1, MRE11, MSH2, MSH6, MUTYH, NBN, PMS1, PMS2, BRIP1, RAD50, RAD51C, STK11 and BARD1. Presence of SNPs in these genes increases the risk of breast cancer and associated diagnostic markers are among the most reliable for assessing prognosis of breast cancer. In this article we reviewed the hereditary genes of breast cancer and SNPs associated with increasing the risk of breast cancer that were recently were reported from candidate gene, meta-analysis and GWAS studies. SNPs of genes associated with breast cancer can be used as a potential tool for improving cancer diagnosis and treatment planning.

• 대한기계학회논문집B
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• 제23권3호
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• pp.299-310
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• 1999

Effect of electrostatic and inertial forces on the pre-charged particle deposition was theoretically and experimentally studied by introducing the inertia impactor subjected to an electric field. To derive the analytic solution, we assumed that a flow was an ideal stagnation flow, a particle had saturation charges, and the electric field within the test section was uniform. On the other hand, $Al_2O_3$ particle groups were used as the test particles, which mean sizes were $1{\mu}m$, $3{\mu}m$, and $5{\mu}m$. To measure the deposition efficiency, the light scattering method was used. The results showed that the deposition efficiency was minimized at a certain nozzle velocity as increasing the nozzle velocity, only if the electric force was applied. As the electric field strength increased, $Stk_{50}{^{1/2}}$ was decreased, and its decreasing rate was reduced with increasing the flow velocity. Moreover the existence of electric field was against the cut-off performance of the inertia impactor.

• International Journal of Aeronautical and Space Sciences
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• 제17권1호
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• pp.89-100
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• 2016

Given the unpredictability of the space environment, satellite communications are manually performed by exchanging telecommands and telemetry. Ground support for orbiting satellites is given only during limited periods of ground antenna visibility, which can result in conflicts when multiple satellites are present. This problem can be regarded as a scheduling problem of allocating antenna support (task) to limited visibility (resource). To mitigate unforeseen errors and costs associated with manual scheduling and mission planning, we propose a novel method based on a genetic algorithm to solve the ground support problem of multiple satellites and antennae with visibility conflicts. Numerous scheduling parameters, including user priority, emergency, profit, contact interval, support time, remaining resource, are considered to provide maximum benefit to users and real applications. The modeling and formulae are developed in accordance with the characteristics of satellite communication. To validate the proposed algorithm, 20 satellites and 3 ground antennae in the Korean peninsula are assumed and modeled using the satellite tool kit (STK). The proposed algorithm is applied to two operation modes: (i) telemetry, tracking, and command and (ii) payload. The results of the present study show near-optimal scheduling in both operation modes and demonstrate the applicability of the proposed algorithm to actual mission control systems.

• Journal of information and communication convergence engineering
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• 제14권3호
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• pp.177-183
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• 2016

A lot of Internet of Things devices has resource-restricted environment, so it is difficult to implement the existing block ciphers such as AES, PRESENT. By this reason, there are lightweight block ciphers, such as SIMON, SPECK, and Simeck, support various block/key sizes. These lightweight block ciphers can support the security on the IoT devices. In this paper, we propose efficient implementation methods and performance results for the Simeck family block cipher proposed in CHES 2015 on an 8-bit ATmega128-based STK600 board. The proposed methods can be adapted in the 8-bit microprocessor environment such as Arduino series which are one of famous devices for IoT application. The optimized on-the-fly (OTF) speed is on average 14.42 times faster and the optimized OTF memory is 1.53 times smaller than those obtained in the previous research. The speed-optimized encryption and the memory-optimized encryption are on average 12.98 times faster and 1.3 times smaller than those obtained in the previous studies, respectively.

• Journal of Astronomy and Space Sciences
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• 제27권2호
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• pp.97-106
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• 2010

To prepare for a Korean lunar orbiter mission, a precise lunar orbit propagator; Yonsei precise lunar orbit propagator (YSPLOP) is developed. In the propagator, accelerations due to the Moon's non-spherical gravity, the point masses of the Earth, Moon, Sun, Mars, Jupiter and also, solar radiation pressures can be included. The developed propagator's performance is validated and propagation errors between YSPOLP and STK/Astrogator are found to have about maximum 4-m, in along-track direction during 30 days (Earth's time) of propagation. Also, it is found that the lifetime of a lunar polar orbiter is strongly affected by the different degrees and orders of the lunar gravity model, by a third body's gravitational attractions (especially the Earth), and by the different orbital inclinations. The reliable lifetime of circular lunar polar orbiter at about 100 km altitude is estimated to have about 160 days (Earth's time). However, to estimate the reasonable lifetime of circular lunar polar orbiter at about 100 km altitude, it is strongly recommended to consider at least $50\;{\times}\;50$ degrees and orders of the lunar gravity field. The results provided in this paper are expected to make further progress in the design fields of Korea's lunar orbiter missions.

• 대한임베디드공학회논문지
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• 제14권6호
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• pp.329-338
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• 2019

Today's embedded software (SW) developments are mostly preceded by composing Software Requirement Specification (SRS). In particular, in the domain of weapon systems, it is essential to have a systematic method for the verification of the SW functionality. To be more specific, it is crucial to check if the SW functionality is implemented as described in SRS, so-called SW suitability verification. Unfortunately, existing static or dynamic SW testing methods are not sufficient to evaluate suitability with SRS since those testings only verify the robustness of the SW codes. In this paper, we propose an automatic embedded SW suitability verification framework which is based on a structured SRS. The major challenge in the automation of this verification framework is how to get rid of ambiguities in SRS. In order to overcome this challenge, we propose a structured SRS description framework and the supporting toolchain for that. We show how the proposed framework is applied to an actual SRS of a weapon system.