• 전기학회논문지
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• 제61권10호
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• pp.1483-1488
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• 2012

This paper analyzed the precision and accuracy of the altitude-aided GNSS using the altitude information from digital map. The precision of altitude-aided GNSS is analysed using the theoretically derived DOP. It is confirmed that the precision of altitude-aided GNSS is superior to the general 3D positioning method. It is also shown that the DOP of altitude-aided GNSS is independent of altitude bias error while the accuracy was influenced by the altitude bias error. Furthermore, it is shown that, since the altitude bias error influenced differently to each pseudorange measurement, the effect of the altitude bias error is more serious than clock bias error which does not influence position error at all. The results are evaluated by the simulation using the commercial RF simulator and GPS receiver. It confirmed that altitude-aided GNSS could improve not only precision but also accuracy if the altitude bias error are small. These results are expected to be easily applied for the performance improvement to the land and maritime applications.

• 환경생물
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• 제38권4호
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• pp.594-602
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• 2020

지형과 고도가 논둑에 서식하는 토양성거미의 군집과 다양성에 미치는 영향을 조사하였다. 지형의 영향평가를 위해 벼재배기에 산간지와 평야지에서 비교한 결과 거미의 군집구조가 달랐으며 발생밀도는 산간지보다 평야지에서 높았다. 늑대거미과가 가장 우점하였으며 이사고늑대거미(P. isago)의 발생밀도는 산간지보다 평야지에서 높았다. 거미군집의 발생은 국지(100 km²) 및 지역(1,000 km²) 범위에서 유사하였다. 고도의 영향과 관련하여 휴한기에 지형이 유사한 장수와 정읍 지역을 비교한 결과 발생밀도는 지역 간 차이가 없었으나, 긴마디늑대거미속(Pardosa spp.) 3종의 발생밀도는 정읍에서 높았다. 이러한 결과는 지형과 고도가 군집 수준에서 토양성 논거미의 다양성지수에 미치는 영향은 크지 않으나, 종 수준에서 논에 의존적인 늑대거미과의 우점종에 영향을 줄 수 있다는 것을 보여준다.

• 전자공학회논문지
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• 제49권10호
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• pp.18-22
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• 2012

본 논문은 GPS 위성의 기하학적 배치 한계로 인한 고도값 오차를 보정하기 위하여 기압고도계를 활용한 고도 데이터의 성능을 향상 시키는 방안을 제시하였고, 보정된 고도데이터의 정확도를 분석하였다. 코드 기반의 상업용 GPS칩은 고도 데이터의 부정확으로 신뢰도가 떨어져 이를 항법 데이터로 활용하지 못하고 있다. 이러한 문제점을 해결하기 위하여 고도 변화를 기반으로 고도를 측정하는 기압고도계로부터 고도의 상대적 변화를 추출하고, GPS 고도계에 반영하여 보정된 고도 데이터를 획득한다. 이를 수치지도의 고도와 비교하여 보정된 고도데이터의 정확도를 검증한다.

• 한국추진공학회지
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• 제20권3호
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• pp.87-95
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• 2016

본 논문에서는 E-D 노즐을 설계하여 고도 보정에 대한 효과와 Throttling에 대한 가능성 연구를 수행하였다. 고도 보정에 대한 효과를 확인하기 위하여 연소실 압력을 일정하게 유지하며, 총 3가지(해수면, 고도 10 km, 고도 16 km)의 외부 대기환경 조건을 이용하여 해석적 연구를 수행하였다. 그 결과 고도가 상승할수록 유효 노즐 출구 면적 역시 점점 증가하였으며 이로 인하여 추력도 증가하였다. 또한 Throttling에 대한 가능성을 파악하기 위하여 핀틀의 위치를 연소실 쪽으로 후진시켜 노즐 목 면적을 작게 모델링하여 해석적 연구를 수행하였다. 일반적인 핀틀 추력기와 동일하게 노즐 목 면적이 줄어들수록 연소실 압력이 상승하며 추력 역시 증가하였다.

• Asian-Australasian Journal of Animal Sciences
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• 제24권2호
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• pp.246-249
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• 2011

The present study was carried out on broilers to study the effect of oral administration of vitamin E and selenium (E-care Se) on growth performance, haematological and biochemical parameters for a period of 42 days (6 weeks). A total of 90 oneday-old broiler chicks were divided into three equal groups: $T_1$, $T_2$ and $T_3$. Group T1 was maintained as control and was fed only with the basal diet throughout the experimental period. Two experimental diets, $T_2$ and $T_3$, were formulated to contain an additional 100 g (150 IU vitamin E/kg+0.5 mg Se/kg) and 200 g (300 IU vitamin E/kg+1.0 mg Se/kg) of E-care Se which was the source of vitamin E and selenium. Body weight was significantly (p<0.05) higher in antioxidant-treated groups compared to the control group. There were no significant differences in feed conversion ratio (FCR). Blood samples were collected from the jugular vein for haematological (TEC, Hb, PCV and ESR) and biochemical (GOT and GPT) study. Body weight was increased significantly in both treated groups compared with the control group and highest body weights were recorded in group $T_2$. TEC, PCV and Hb content increased significantly (p<0.01) in the treated groups as compared to the control group, but ESR, GOT and GPT values decreased significantly (p<0.01) in both treated groups as compared to the control group. The result reveals that use of antioxidants (vitamin E and selenium) is an effective way of getting the best result in terms of body weight gain and haemato-biochemical profiles in broiler birds at high altitude.

• 한국태양에너지학회:학술대회논문집
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• 한국태양에너지학회 2012년도 춘계학술발표대회 논문집
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• pp.134-139
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• 2012

This study observed downward long and short-wave radiant environment with selecting 4 areas which have different height in downtown and 1 suburban area to figure out the characteristic of radiant environment in each altitude. The purpose of this study is to collect the preliminary data for interpreting urban thermal environment in summer season by analyzing thermal characteristic of atmosphere in the upper of downtown. The results of this study are as follows. 1) The higher altitude has the lower temperature, and temperature difference was more huge in day time than night time. 2) The short wave radiation according to altitude was higher as altitude was high. 3) Generally, the higher altitude has the lower air temperature, and also the higher altitude has the lower downward long wave radiation by the atmospheric radiation. 4) The ratio short wave radiation of long wave radiation was lower as altitude was high. And the urbanization effect was higher as the ratio was low.

• 한국군사과학기술학회지
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• 제12권5호
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• pp.683-688
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• 2009

A research was conducted about the Reynolds number effect on the projectile with an altitude change. The atmosphere conditions change in accordance with an altitude change. It effects the Reynolds number. To confirm how the phenomena affect the trajectory of the projectile, a computer program is designed with an altitude and a range considered. The MISSILE DATCOM which is based on the semi-empirical method was utilized to get aerodynamic coefficients. The result shows that the Reynolds number considerably changes as the altitude change. It causes to change the drag coefficient of the projectile. As the Reynolds number decreases, the skin friction drag increases significantly. It causes to decrease the maximum altitude and the range.

• Journal of Electrical Engineering and Technology
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• 제10권2호
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• pp.625-633
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• 2015

The effect of altitude on thermal conduction, surface temperature, and thermal radiation of partial arc was investigated on the basis of molecular gas dynamics to facilitate a deep understanding of the pollution surface discharge mechanism. The DC flashover model was consequently modified at high altitude. The validity of the modified DC flashover model proposed in this paper was proven through a comparison with the results of high-altitude simulation experiments and earlier models. Moreover, the modified model was found to be better than the earlier modified models in terms of forecasting the flashover voltage. Findings indicated that both the thermal conduction coefficient and the surface thermodynamics temperature of partial arc had a linear decrease tendency with the altitude increasing from 0 m to 3000 m, both of which dropped by approximately 30% and 3.6%, respectively. Meanwhile, the heat conduction and the heat radiation of partial arc both had a similar linear decrease of approximately 15%. The maximum error of DC pollution flashover voltage between the calculation value according to the modified model and the experimental value was within 6.6%, and the pollution flashover voltage exhibited a parabola downtrend with increasing of pollution.

• Journal of Astronomy and Space Sciences
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• 제36권3호
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• pp.213-223
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• 2019

This paper analyzes delta-Vs to maintain an extremely low altitude on the Moon and investigates the possibilities of performing a CubeSat mission. To formulate the station-keeping (SK) problem at an extremely low altitude, current work has utilized real-flight performance proven software, the Systems Tool Kit Astrogator by Analytical Graphics Inc. With a high-fidelity force model, properties of SK maneuver delta-Vs to maintain an extremely low altitude are successfully derived with respect to different sets of reference orbits; of different altitudes as well as deadband limits. The effect of the degree and order selection of lunar gravitational harmonics on the overall SK maneuver strategy is also analyzed. Based on the derived SK maneuver delta-V costs, the possibilities of performing a CubeSat mission are analyzed with the expected mission lifetime by applying the current flight-proven miniaturized propulsion system performances. Moreover, the lunar surface coverage as well as the orbital characteristics of a candidate reference orbit are discussed. As a result, it is concluded that an approximately 15-kg class CubeSat could maintain an orbit (30-50 km reference altitude having ${\pm}10km$ deadband limits) around the Moon for 1-6 months and provide almost full coverage of the lunar surface.

• 한국대기환경학회지
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• 제34권3호
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• pp.486-492
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• 2018

Black carbon concentrations were measured along the altitude at various locations using a drone coupled with a small black carbon detector. The measurement locations are Eunseok Mountain, downtown, four places in KOREATECH campus, Byeongcheon, Cheonan, Chungcheongnam-do, and Chungbu Expressway in Ochang-eup, Cheongju, Chungcheongbuk-do. The average concentration of black carbon measured in Eunseok Mountain was $1.64{\mu}g/m^3$ and the average concentration near the Chungbu Expressway was measured to be $3.86{\mu}g/m^3$. The average concentrations of four places inside campus ranged from 1.37 to $2.67{\mu}g/m^3$. The concentration of black carbon at all places tended to be slightly decreased according to the altitude, but the influence of pollution source, geometry, wind speed, and wind direction are thought to be larger than the effect of altitude. Effect of air flow caused by drone flight on the measurement of black carbon were investigated and it resulted in that the measurement of BC concentration was affected by less than 5%.