• Journal of Astronomy and Space Sciences
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• 제13권2호
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• pp.105-116
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• 1996

이 연구는 1992년 8월 11일과 1993년 9월 26일 발사된 우리별 1호 및 우리별 2호의 열제어 모델 및 그 동안의 운용 결과에 대한 해석을 바탕으로 한 것이다. 우리별 1, 2호는 아리안 발사체의 초소형 위성 탑재를 위한 특수 구조물에 장착되어 발사되었기 때문에 크기, 전력, 무게 등의 제한으로 인해 외부로부터의 열 흡수와 방출의 제어 및 내부의 연결 모듈간의 열 흐름을 제어하여 위성체 전반의 열적 환경을 조절하는 수동적인 방식의 열제어를 채택하게 되었다. 우리별 위성의 주 임무는 위성 기술의 개발과 더불어 위성체 바닥면에 탑재된 CCD 카메라를 이용하여 지구 표면을 촬영하는 것이었기 때문에 위성의 바닥면은 항상 지구의 중심을 향하고 있게 된다. 이 연구는 위성의 임무 궤도에 대한 분석으로부터 열 모델링, 시뮬레이션 결과 및 우리별 2호의 실제 운용헤서 얻어진 원격검침 정보를 바탕으로 한 열 모델의 평가를 포함한다. 이 분석 결과를 바탕으로 수동 제어에 의한 우리별 위성의 열 모델 및 해석이 실제 측정된 온도 데이터와 평균 오차 $$10^{\circ}C$ 이내에서 일치되었음을 보여 준다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2013년도 춘계학술대회 논문집
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• pp.390-394
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• 2013

고정밀 광학계를 탑재한 관측 위성은 매우 높은 지향 안정성을 요구하지만 인공위성의 자세 제어를 위해 사용하는 반작용 휠, 극저온 냉각을 위한 cooler 등 다양한 진동원에 의해 미소 진동이 발생할 수 있다. 고정밀 탑재체를 외부 진동으로부터 보호하기 위한 가장 일반적인 방법은 진동이 전달되는 경로에 진동 절연장치를 도입하는 것이다. 본 논문에서는 미소진동 절연을 위한 1 축 능동 진동 절연장치의 개발 및 진동 절연 성능 시험을 기술하였다. 개발한 절연장치의 고유진동수를 조절하기 위해 원하는 강성을 갖는 membrane 구조를 설계하였으며 능동 제어를 위해 전자석을 사용하였다. 절연장치의 성능 시험 결과를 통해 능동 제어 시 고주파수 대역에서 절연성능의 저하 없이 공진의 크기를 줄일 수 있는 것과 개발된 진동 절연 장치가 미소 진동을 효과적으로 절연할 수 있는 것을 확인하였다.

• 대한유전성대사질환학회지
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• 제11권1호
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• pp.88-98
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• 2011

Lesch-Nyhan syndrome is a X-linked recessive disorder caused by a deficiency of the enzyme hypoxanthine-guanidine phosphoribosyltransferase (HPRT), enzyme to recycle purines. Case history: born induced vaginal delivery at 40 weeks complicated by premature membrane ruputure, body weight 2.820 gm. He showed failure to thrive showing severe protein aversion like milk products and pink daper. Developmental delay revealing rolling over at 10.5 month, followed by regression. Seizure at 2 months, His poor oral feeding was lifelong problem. Weak crying, spastic, choreoathetoid movement. Self mutilating behavior noted and diagnosed at age 3 years. No family history of consanguinity and neurological disorders. Method: Laboratory test, physical exam, imaging study and molecular. Clinical follow up Treat ment with allopurinol. Result: uric acid 10.5 mg/dL (N 3.5-7.9), APRT 151.1uM/ min/ml pro(25.7-101), HPRT 7.6 (N 233.5-701) and c.151C>T hemizygote (p,Arg51X). Abdominal sonogram showed staghorn calculi in both kidneys, brain MRI brain atrophy. Clinical follow up showed, seizure at 2 mo, developmental delay (head control and, rolling over at at 11mo, pointing body part at 2 yr 7 mo, eye hand coordination at 2 y 11mo,creeping at 3 y 7 mo, speaking words at 6 y 6 mo ),and developmental regression at 3 yr of age. Sleeping problem including insomnia and severe constipation. Self mutilating behavior (lip bite) started at 2.5 yr, neurologic sx including intermittent upward gaze accompanied by swallowing difficulty at 3 y 7 mo grand mal seizure at 4.5 yr and spastic extremity and trunchal hypotonia and choleoathetoid movement and ataxia at 6.5 yr. Scoliosis with severe spasticity at 9 yr 9 mo. Acute life threatening episode with irregular breathing at 9 yr and 9 mo, Emaciation and nephrolithiasis and recurrent pneumonia. Died suddenly at 10 yr 3 mo. Conclusion: life long feeding problem, chronic gut motility dysfunction, sleeping difficulty and progressing neurologic deterioration and nephrolithiasis despite normal serum uric acid maintence by allopurinol treatment.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 1998년도 Proceedings of International Symposium on Remote Sensing
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• pp.301-306
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• 1998

Korea Aerospace Research Institute (KARI) is developing a Korea Multi-Purpose Satellite I (KOMPSAT-I) which accommodates Electro-Optical Camera (EOC), Ocean Scanning Multi-spectral Imager (OSMI), and Space Physics Sensor (SPS). The satellite has the weight of about 500kg and will be operated on the 10:50 AM sun-synchronized orbit with the altitude of 685 km. The satellite will be launched in 1999 and its lifetime is expected to be over 3 years. The main mission of EOC is the cartography to provide the images from a remote earth view for the production of 1/25000-scale maps of KOREA. EOC collects 510 ~ 730 nm panchromatic imagery with the ground sample distance(GSD) of 6.6 m and the swath width of 17 km by push broom scanning. EOC also can scan $\pm$45 degree across the ground track using body pointing method. The primary mission of OSMI is worldwide ocean color monitoring for the study of biological oceanography. It will generate 6 band ocean color images with 800 km swath width and 1km GSD by whiskbroom scanning. OSMI is designed to provide on-orbit spectral band selectability in the spectral range from 400 nm to 900 nm through ground command. This flexibility in band selection can be used for various applications and will provide research opportunities to support the next generation sensor design. SPS consists of High Energy Particle Detector (HEPD) and ionosphere Measurement Sensor (IMS). HEPD has missions to characterize the low altitude high-energy Particle environment and to study the effects of radiation environment on microelectronics. IMS measures densities and temperature of electrons in the ionosphere and monitors the ionospheric irregularities at the KOMPSAT orbit.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 1998년도 Proceedings of International Symposium on Remote Sensing
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• pp.313-318
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• 1998

Electro-Optical Camera(EOC) is the main payload of Korea Multi-Purpose SATellite(KOMPSAT) with the mission of cartography to build up a digital map of Korean territory including Digital Terrain Elevation Map(DTEM). This instrument which comprises EOC Sensor Assembly and EOC Electronics Assembly produces the panchromatic images of 6.6 m GSD with a swath wider than 17 km by push-broom scanning and spacecraft body pointing in a visible range of wavelength, 510 ~ 730 nm. The high resolution panchromatic image is to be collected for 2 minutes during 98 minutes of orbit cycle covering about 800 km along ground track, over the mission lifetime of 3 years with the functions of programmable rain/offset and on-board image data storage. The image of 8 bit digitization, which is collected by a full reflective type F8.3 triplet without obscuration, is to be transmitted to Ground Station at a rate less than 25 Mbps. EOC was elaborated to have the performance which meets or surpasses its requirements of design phase. The spectral response the modulation transfer function, and the uniformity of all the 2592 pixel of CCD of EOC are illustrated as they were measured for the convenience of end-user. The spectral response was measured with respect to each gain setup of EOC and this is expected to give the capability of generating more accurate panchromatic image to the EOC data users. The modulation transfer function of EOC was measured as greater than 16% at Nyquist frequency over the entire field of view which exceeds its requirement of larger than 10%, The uniformity that shows the relative response of each pixel of CCD was measured at every pixel of the Focal Plane Array of EOC and is illustrated for the data processing.

• 한국소음진동공학회논문집
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• 제22권11호
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• pp.1042-1048
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• 2012

A 2-axis gimbal system is one of main disturbance sources affecting image jitter response of a satellite. The gimbal system comprises azimuth stage and elevation stage, and these pointing mechanism can be rotated by stepping motors about its azimuth and elevation axes simultaneously. Because of the complex and coupled dynamic motion of the gimbal system, its moment of inertia and structural modes can be changed according to the system configuration, and thus the gimbal system generates complicated and non-linear disturbance characteristics. In order to improve the jitter response of a spacecraft, it is an indispensable process to reduce the micro-vibration disturbance level of the antenna system. In the present research, a 2-axis gimbal system was manufactured and then its micro-vibration test was performed in terms of two types of stepping motors(2-phase and 5-phase). The test results show that the disturbance level of the gimbal system can be reduced by replacing the 2-phase stepping motor with the 5-phase one, and the average disturbance attenuation ratio is 56 % in peak level and 48 % in standard deviation level. The experimental results confirm that it is an efficient jitter reduction method to adopt a high-phase stepping motor.

• 한국항공운항학회지
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• 제17권3호
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• pp.1-6
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• 2009

Since the success of the first flight, vast advancements have been made to the aircrafts with recent developments incorporating highly complex mechanisms, placing greater emphasis on the competence of the pilot. Studies are currently being undertaken to effectively source the trainee pilots with the most ideal level of aptitude for aviation with an aim to optimise the selection process with focus on economy and time, while research into identifying the optimal human characteristics for aviation is being done. As part of the selection process, number of tests is arranged with focus on the individual competence, suitability for flight, health status, aptitude and intelligence with the results of the tests used as reference materials during the selection procedure. This study has investigated the effect the academic competence has on the aptitude for aviation amongst many other abilities of human beings and the findings show that higher levels of aptitude have been demonstrated by the students who have displayed academic excellence across all the courses with statistics pointing to a positive correlation between the two subjects. This supports the theory that students who are academically superior have higher probability of being found to possess greater level of flight aptitude. The outcome of the study iterates the fact that academic competence of the students should not be regarded lightly in the selection process. Based on the current study, it is believed that a research into determining the relationship between the SAT results, average yearly grade and flight aptitude will help identify the key factors in possessing high level of flight aptitude with greater certainty.

• 한국항공우주학회지
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• 제42권9호
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• pp.779-788
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• 2014

저궤도 위성이 제한된 전력 내에서 임무를 성공적으로 수행하기 위해서는 효율적인 전력생산이 중요하다. 이를 위해 저궤도 소형위성의 전력계에서는 주로 MPPT (Maximum Power Point Tracking) 방식을 사용하여 태양전지에서 생산되는 전력을 조절한다. 본 연구에서는 소형 큐브위성(KAUSAT-5)에 적용될 퍼지 로직 기반의 MPPT 알고리즘을 제안하며, 제안된 방법의 유용성을 확인하기 위해 MATLAB/Simulink와 STK (Systems Tool Kit)를 연동하여 시뮬레이션을 수행하였다. Simulink와 STK를 이용하여 위성 궤도와 자세에 따른 태양 광량과 운용모드에 따라 변하는 부하용량에 대해 KAUSAT-5의 두 가지 지향모드에서 EBA(Energy Balance Analysis)를 수행하였고, 이를 통해 제안된 퍼지 로직 기반의 MPPT 알고리즘의 성능을 확인하였다. 제안된 퍼지 로직 기반의 MPPT는 가장 일반적인 방법의 하나인 P&O (Perturbation & Observation)와 성능을 비교하여 유용성을 확인하였다.

• 한국정보과학회논문지:정보통신
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• 제32권6호
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• pp.723-731
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• 2005

오늘날 인프라 무선 랜은 많은 사용자들이 사용하는 중요한 인터넷 접속 기술이다. 지금까지 무선 랜에 관한 연구들은 물리 계층의 채널 다양성으로 인하여 발생하는 모델링 부정확성에 대해 충분히 고려하지 않고, MAC 프로토콜의 향상 및 분석 그리고 시뮬레이션을 통한 성능 평가에만 초점을 맞추어 왔다. 본 논문에서는 계층 상호 간의 의존성의 중요성에 주목하는 새로운 시각으로 IEEE 802.11 무선 랜의 특성을 고찰한다. 실제 무선 랜 시스템 상에서 실험을 수행하여 물리 계층에서 발생하는 불평등성을 관찰하였다. 그리고, 그것이 노드들 간의 혼잡 수준을 떨어뜨리는 역할을 하여 경쟁 기반의 MAC 처리율이 혼잡 상태에서도 서서히 감소하는 것을 보인다. 반면에 노드들 간의 공평성과 노드 처리율의 안정성은 시스템 입력 로드가 특정 수준을 넘으면 크게 저하되는 것을 보인다. 이와 같은 결과를 통하여, 처리율을 높이기 위해 링크 계층에서 제어를 할 필요성은 적은 반면에, 공평한 자원 분배나 서비스의 품질을 보장하기 위해서는 트래픽 제어가 필요하다는 것을 알 수 있다. 시스템의 성능 평가를 위하여 시뮬레이션과 실험을 병행하였다.

• Journal of Crop Science and Biotechnology
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• 제11권4호
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• pp.257-262
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• 2008

Genetic diversity of cultivated wheat is narrowing down and is increasingly becoming non-complacent in tackling new pathogenic races and adverse environmental situations. Wild relatives of wheat are rich repositories of beneficial genes that are capable of defying adverse situations. However, these wild species are not readily crossable with cultivated ones. The present study attempted to cross three wild wheat species as females with three cultivated species of varying ploidy to understand the intricate behaviour of hybrids in relation to cytology, morphology, and molecular recombination. Post-fertilization barriers caused hybrid recovery in wild species in contrast to cultivated species. Triticum monococcum did not produce hybrids in any of the crosses. Various degrees of chromosome anomalies and hybrid sterility were seen with hybrids of T. timopheevi and T. sphaerococcum. Cytoplasmic factors were suspected to add more to the abnormality. G genome from T. timopheevi could enhance more pairing between Band D of cultivated species. Precocity of certain chromosomes in laggard formation was evident, pointing towards evolutionary self balance of the genomes which prevented homeologous pairing. They are eliminated in hybrids. Molecular diversity clearly corroborated with genetic proximity of the species, which distinguished themselves by maintaining the genome homeology.