• 농촌계획
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• 제17권3호
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• pp.81-90
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• 2011

The altitude criteria of 'Management of Mountains District Act' and 'National Land Planning and Utilization Act' are different because the adaptive reuse permissions on mountains district by two acts have been operated individually and each criteria has some problems for application. This study aims to suggest proposals for improvements of altitude criteria by two acts. The altitude criteria of the duel legal systems were researched by literature review and inherent issues were derived by interview with public officers and GIS tools applied to cases. The results are as follows : First, duel criteria systems need to be integrated based on the format by 'Management of Mountains District Act'. Second, the criteria index(50/100) by 'Management of Mountains District Act' need to be adjusted due to the preserved area ratio in mountains district and the each definition of 'the peak point of the mountain' and 'the tail of the mountain' can be changed as 'the highest point within the same slope(including ridge)' and as 'the average of the highest and the lowest point on boundary between the mountain district and the other land use district'. Third, the method of slope division may be determined by the conditions of local areas and the discrepancy between the two slopes in common boundaries must be adjusted. Finally, the maps containing preservation areas and development areas need to be notified.

• 항공우주시스템공학회지
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• 제10권2호
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• pp.7-13
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• 2016

Multi disciplinary approach for aerodynamics, structure, propulsion, and flight control system is necessary to develop High Altitude Long Endurance Unmanned Aerial Vehicles (HALE UAV). Various HALE UAV development trends are surveyed to understand their operational requirements. Separating the UAV Take Off Weight by 150kg, Airworthiness implementation direction for HALE UAV is studied under the current Airworthiness regulations. NATO STANAG 4671 and STANAG 4703 Airworthiness certification criteria are analyzed, and their applicability was proposed for future HALE UAV development. In addition, minimization of the risk for UAV is studied by considering probability of cumulative catastrophic failure for HALE UAV. This Hazard Risk Index can support the future UAV Airworthiness Certification Criteria.

• 반도체디스플레이기술학회지
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• 제9권1호
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• pp.67-71
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• 2010

Head up display’s cooling system is auto-diagnosed resulting from the external environment. The quantity of heat depending on this Head up display’s cooling system layout determines the speed of FAN for system cooling. In other words, a system’s heat quantity is planned through the air density depending on altitude, the amount of wind in air depending on FAN control condition, and the algorithm that is proportional to delta temperature. To detect the altitude, we use the criteria of delta T, which is determined by the subtracted value of LED junction temperature, and atmospheric temperature that is recorded on the Head up display system. Depending on the classification of delta T value, the altitude section is determined. While we can use GPS as the tool to detect the altitude, we should predict the change of the air density as the altitude alters, and should not just measure the altitude. And the value of delta T is used as the criterion of detecting the altitude for increasing the cooling efficiency of the car’s inner Head up display system with reflecting the speed of the FAN dependent upon the air density. In our theory, altitude is depending on the value of delta T and stabilizing or maintaining the system’s temperature by changing FAN’s rpm depending on determined value of altitude.

• Journal of Communications and Networks
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• 제8권2호
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• pp.175-181
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• 2006

This paper addresses an in-depth analysis of the stratosphere-to-Earth co-channel interference produced by high-altitude platforms (HAPs) and proposes a new methodology for the evaluation of its impact to terrestrial systems in terms of fractional degradation in performance, taking into account parameters such as HAP's mobility, realistic distribution of azimuth and elevation angles of the terrestrial microwave links (TMLs), and gradual high-altitude platform network (HAPN) loading. Simulations performed for different HAPN configurations, prove that the implementation of the methodology proposed, may lead to a more efficient use of the spectrum shared between the two services.

• 한국군사과학기술학회지
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• 제22권2호
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• pp.151-161
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• 2019

In this study, to evaluate the High Altitude Electromagnetic Pulse(HEMP) protection performance of UHPC/CNT composites by the content of Carbon nanotubes(CNTs), Electromagnetic Shielding Effectiveness(SE) test was performed based on MIL-STD-188-125-1. And the results were verified by applying the Antenna theory. In the case of UHPC with a thickness of 200 mm mixed with 1 % CNT of cement weight, the SE was 28.98 dB at 10 kHz and 45.94 dB at 1 GHz. Then the Scabbing limit thickness for bullet proof was computed based on the result of compressive strength test which was 170 MPa, and it was examined whether it satisfied the HEMP protection criteria. As a result, the required HEMP shielding criteria were satisfied in all frequency ranges as well as the scabbing limit thickness was reduced by up to 43 % compared with that of ordinary concrete.

• 한국전자파학회논문지
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• 제25권2호
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• pp.199-207
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• 2014

고 고도 전자기 펄스(HEMP: High-altitude Electromagnetic Pulse)용 필터는 펄스 전류 주입(PCI: Pulsed Current Injection) 인수시험을 통해 인수기준을 충족하더라도, 실제 부하 장비를 연결하여 장비 운용 상태에서 실시하는 PCI 검증 시험수행 시에는 부하 장비의 전자기 전도 내성 수준에 따라서 장비가 손상될 수도 있다. 본 논문에서는 HEMP 방호시설에서 PCI 검증 시험 수행이 어려운 경우, 이에 대한 방안으로서 HEMP 필터의 PCI 인수시험 잔류 전류 측정값과 부하 장비의 과도 전자기 전도 내성 기준 값에 대한 특성인자(norm) 비교를 통해 필터 잔류 전류가 부하 장비에 미치는 영향분석 방법을 제안하였다. C4I(Command, Control, Communications, Computer, and Intelligence) 쉘터용으로 제작된 HEMP 필터와 쉘터 탑재장비를 활용하여 HEMP 필터 PCI 인수시험, 과도 전자기 전도 내성 시험 및 PCI 검증 시험을 수행하였고, 결과를 분석하였다.

• 한국의류학회지
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• 제20권6호
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• pp.1027-1038
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• 1996

The decision making procedure of consumer's post purchase is important because post purchase evaluation function is the physiological variables in repurchasing. The previous studies of post-purchase decision making showed that consumer compared the expectation of pre-buying with the performance of the product of post-buying. After consumers evaluates the products, consumer is satisfactory or dissatisfactory with products. And the satisfaction effects repurchase intention. The criteria which consumer didn't consider can be important to consumer after buying. Therefore the research problems are as follows; 1. To reveal the consumer's post-purchase clothing evaluative criterita and to indentify the dimensions of post-purchase clothing evaluative criteria. 2, To examine a causal model of the repurchase intention by post- purchase clothing evaluative criteria, satisfaction and brand attitude, A questionnaire was developed and administered 530 women living in Taejeon, and social daytime wear was selected as a clothing item for the study. Consumer's post-purchase clothing evaluative criteria were composed of six dimensions; Fit, Utility, Management, Transformation, Wearing/sewing, Esthetic factor. The main causal model of repurchase intention is that post-purchase clothing evaluative criteria - satisfaction - brand altitude - repurchase intention. Finally we found that the post-purchase clothing evaluative criteria were important because the repurchase intention depended on post-purchase clothing evaluation, too.

• 한국항공운항학회지
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• 제22권1호
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• pp.22-31
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• 2014

Military UAV(Unmanned Aerial Vehicle) operated as a RC(Remotely Control) model level within the limit of the military special use airspace until now. However, the high and medium altitude of URA(Unmanned Reconnaissance Aircraft) which the ROKAF have been trying to import recently is at the UAV level and needs the criteria for the classified airspace flights. The required flight criteria includes operator location, mission operation limit, equipment, etc., which are the principle and standard applied based on the airspace use for UAV. Also, the general flight rules, visual flight rules, instrument flight rules are required in order to have to be applied to the actual flight. Besides, an appliance regulation needs to be arranged regarding two-way communication, ATC and communication issue, airspace and area in-flight between UAS( Unmanned Aircraft System) users. An operation of the UAV in the air significantly requires the guarantee of the aircraft's capacity, and also the standardized flight criteria. A safe and smooth use is ensured only if this criteria is applied and understood by the entire airspace users. For the purpose, a standardized military UAV flight operations criteria that is to be applied for each airspace by UAV is to be prepared through analysis of the present state, a legend UAV system, and a special character analysis.

• 한국항행학회논문지
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• 제7권1호
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• pp.22-29
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• 2003

본 논문에서는 성층권 통신 시스템(HAPS : High Altitude Platform System)과 NGSO (Non-Geostationary Orbit) 시스템간 간섭 영향을 두 가지의 경우로 나누어서 분석한다. 한가지는 HAPS 시스템이 NGSO 시스템에 미치는 간섭이며, 다른 한가지는 NGSO 위성이 HAPS 시스템에 미치는 간섭 영향이다. 그 결과 NGSO 이동국이 받는 간섭은 NGSO 위성 위치가 $95^{\circ}$일 때 가장 높게 나타났으며, 이때 HAPS와 NGSO 모두에 의한 간섭은 사용자 수가 20명 이상부터 간섭 기준을 초과함을 알 수 있었다. 그리고 HAPS 이동국이 받는 간섭의 경우에는 NGSO 위성 앙각이 $87^{\circ}$일 때 가장 높은 간섭이 나타났으며, 이 때 NGSO와 HAPS 모두에 의한 간섭은 사용자 수가 10명 이상부터 간섭 기준을 초과함을 알 수 있었다. 또한 $64^{\circ}$일 때 가장 낮은 간섭이 나타났으며, 이때 NGSO와 HAPS의 사용자 수가 같을 경우에는 190명에서부터 간섭을 초과함을 알 수 있었다.

• 한국지구과학회지
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• 제41권5호
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• pp.459-468
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• 2020

본 연구에서는 2016-2017년 봄철(3-5월) 동안 보성 지역에서의 해풍 발생 시 연직 기상 특성을 분석하기 위해, 해풍 발생에 대한 선정 기준을 마련하였다. 이를 위해 지상에서 측정된 강수량, 운량, 풍향과 지상과 해상 기온의 차이, 1km 고도에서의 윈드프로파일러 및 수치모델 자료를 이용한 풍속 값이 사용되었다. 선정 기준에 따라 보성지역에서의 해풍일을 분류하였고, 해풍 발생 시간 및 고도와 풍속의 크기 분석을 통해 해풍의 시공간적 특성을 파악하였다. 해풍의 발생일은 총 183일 중 23일(12%)로서, 보성지역의 경우 봄철 10일 중 최소 1.2일은 해풍이 나타났다. 해풍은 1200 LST부터 1800 LST로 낮 시간에 지상에서부터 700 m 고도까지 주로 발생하였다. 또한, 최대 풍속은 평균 4.9 m s^-1로 1600 LST에 40 m 고도에서 나타나, 선행연구보다 비교적 낮은 값을 보였다. 이는 해안지형이 복잡하여 지형 효과에 따른 풍속 감소로 인한 것으로 보인다.