• 한국국방경영분석학회지
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• 제34권1호
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• pp.31-45
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• 2008

본 연구는 시스템엔지니어링적 접근방법을 통한 저고도 방공자동화체계의 운용아키텍처 개발을 기술한다. 미래 전장은 단일전구 내에서 다수의 다양한 센서체계와 슈터체계가 각각의 그리드를 형성하고, 네트워크기반 전장관리에 의해 지휘통제(C2: Command and Control)되는 신복합시스템 개념으로 변화하고 있다. 미래 위협은 UAV나 순항미사일 그리고 전술탄도미사일과 같이 전략적 효과가 큰 무인 항행체의 사용으로 특성화 될 수 있으며, 저고도 스텔스 순항미사일과 같은 새로운 위협이 등장하게 될 것이다. 이러한 미래 위협에 대한 저고도방공 운용개념 설정은 시스템엔지니어링 기반의 복합적이고 통합적인 접근방법이 요구된다. 이러한 관점에서 본 연구는 임무 및 미래 운용환경의 식별을 통해 운용시나리오를 작성하고 운용요구사항을 도출했으며, 컴퓨터지원 시스템엔지니어링도구인 CORE 5.0을 사용하여 네트워크기반의 저고도 방공자동화체계의 운용아키텍처를 제시했다.

• 전기전자학회논문지
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• 제22권3호
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• pp.747-753
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• 2018

Currently, many companies have succeeded in logistics delivery experiments utilizing drone and report it. When a drone is used commercially, long-term flight is an important performance that a drone should have. However, unlike vehicles operated on the ground, drone is a vehicle that continues to consume energy when maintaining the current altitude or moving to the destination. Therefore, the drones can fly for a long time as the capacity of the battery is large, but the batteries with large capacity are restricted by heavy weight and it acts as a limiting factor in a commercial use. To address this issue, we attempt to compare how far we can fly than forward flight based on the flight pattern with the same energy consumption condition. In this paper, the comparison of energy consumption was performed in three flight pattern, forward flight without altitude change and forward flight with altitude change, by computer simulation and it shows the increasing of flight distances when the quadrotor fly with altitude change from high altitude to low altitude.

• 한국군사과학기술학회지
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• 제20권3호
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• pp.345-351
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• 2017

A wind tunnel test for the scaled parachute models was performed to verify aerodynamic characteristics for practical usage of Korean low cost low altitude aerial delivery system. The cruciform shaped cargo parachute models for heavy and light weight were ejected into wind tunnel test section; and the drag forces acting on the models in steady condition were measured in accordance with velocity. Also, the maximum opening forces during inflation were obtained and captured by a high speed camera to analyze the inflation characteristics and evaluate the design of the low cost aerial delivery system. The results showed a reliable stability and met the design requirement of delivery operation system for R.O.K Air Force.

• International Journal of Advanced Culture Technology
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• 제8권1호
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• pp.173-181
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• 2020

This study examines whether unmanned aircraft systems (UAS) operated in the context of UAS traffic management (UTM) can be properly operated in its flight environment. In detail, this study examines the influencing navigation factors affecting UASs during flight and examines factors affecting the navigation of UASs under UTM. After deriving various factors affecting navigation, their importance are determined by applying the analytic hierarchy process technique, and the important influencing factors are examined. For low-altitude UAS navigation, errors are classified into navigation-system and flight-technical errors, and a hierarchy is constructed for their sub-factors affecting the influencers. Through this, influencing factors for precise navigation of low-altitude UAS are analyzed, and high importance items are identified.

• 한국측량학회:학술대회논문집
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• 한국측량학회 2010년 춘계학술발표회 논문집
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• pp.249-250
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• 2010

The study aims to propose a method that shall rapidly acquire 3D spatial information of the frequently changing city areas by using the low altitude aerial images taken by the UAV. The artificial 3D model of the artificial structures was constructed using the aerial image data photographed at the test area, calibration data of the non-metric camera and the results of the ground control point survey. Also, the digital surface model was created for areas that were changed due to a number of civil works. Through the above studies, the possibilities of constructing a 3D virtual city model, renewal of 3D GIS database, abstraction of changed information in geographic features and on-demand updating of the digital map were suggested.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년도 제31회 추계학술대회논문집
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• pp.153-156
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• 2008

고공 환경에서의 점화 연소 특성을 확인하기 위해 선행되어야 할 저압/저온 환경 모사 및 연료 유량 제어 실험을 수행하였다. 저압 환경을 모사하기 위하여 초음속 디퓨저를 이용하였고, 공기 유량 공급 및 디퓨저 1차 전단 노즐 압력에 따라 다양한 고도의 저압 환경을 조성할 수 있음을 확인하였다. 또한 저온 환경을 모사하기 위해 액체 질소를 이용한 열교환기를 활용하였고, 혼합 탱크로 유입되는 극저온/상온 공기 온도 조건을 일정하게 유지할 경우 다양한 공기 유량 조건에서 혼합 공기의 온도는 극저온/상온 공기의 혼합비에 의해 결정됨을 알 수 있었다. 이에 따라 본 연구에서 구축한 고고도 환경 모사 시스템을 활용하여 다양한 고도 조건에서의 점화 및 연소 특성 실험 수행이 가능함을 입증하였다.

• 운동영양학회지
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• 제16권2호
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• pp.65-71
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• 2012

Oxygen is the final acceptor of electron transport from fat and carbohydrate oxidation, which is the rate-limiting factor for cellular ATP production. Under altitude hypoxia condition, energy reliance on anaerobic glycolysis increases to compensate for the shortfall caused by reduced fatty acid oxidation [1]. Therefore, training at altitude is expected to strongly influence the human metabolic system, and has the potential to be designed as a non-pharmacological or recreational intervention regimen for correcting diabetes or related metabolic problems. However, most people cannot accommodate high altitude exposure above 4500 M due to acute mountain sickness (AMS) and insulin resistance corresponding to a increased levels of the stress hormones cortisol and catecholamine [2]. Thus, less stringent conditions were evaluated to determine whether glucose tolerance and insulin sensitivity could be improved by moderate altitude exposure (below 4000 M). In 2003, we and another group in Austria reported that short-term moderate altitude exposure plus endurance-related physical activity significantly improves glucose tolerance (not fasting glucose) in humans [3,4], which is associated with the improvement in the whole-body insulin sensitivity [5]. With daily hiking at an altitude of approximately 4000 M, glucose tolerance can still be improved but fasting glucose was slightly elevated. Individuals vary widely in their response to altitude challenge. In particular, the improvement in glucose tolerance and insulin sensitivity by prolonged altitude hiking activity is not apparent in those individuals with low baseline DHEA-S concentration [6]. In addition, hematopoietic adaptation against altitude hypoxia can also be impaired in individuals with low DHEA-S. In short-lived mammals like rodents, the DHEA-S level is barely detectable since their adrenal cortex does not appear to produce this steroid [7]. In this model, exercise training recovery under prolonged hypoxia exposure (14-15% oxygen, 8 h per day for 6 weeks) can still improve insulin sensitivity, secondary to an effective suppression of adiposity [8]. Genetically obese rats exhibit hyperinsulinemia (sign of insulin resistance) with up-regulated baseline levels of AMP-activated protein kinase and AS160 phosphorylation in skeletal muscle compared to lean rats. After prolonged hypoxia training, this abnormality can be reversed concomitant with an approximately 50% increase in GLUT4 protein expression. Additionally, prolonged moderate hypoxia training results in decreased diffusion distance of muscle fiber (reduced cross-sectional area) without affecting muscle weight. In humans, moderate hypoxia increases postprandial blood distribution towards skeletal muscle during a training recovery. This physiological response plays a role in the redistribution of fuel storage among important energy storage sites and may explain its potent effect on changing body composition. Conclusion: Prolonged moderate altitude hypoxia (rangingfrom 1700 to 2400 M), but not acute high attitude hypoxia (above 4000 M), can effectively improve insulin sensitivity and glucose tolerance for humans and antagonizes the obese phenotype in animals with a genetic defect. In humans, the magnitude of the improvementvaries widely and correlates with baseline plasma DHEA-S levels. Compared to training at sea-level, training at altitude effectively decreases fat mass in parallel with increased muscle mass. This change may be associated with increased perfusion of insulin and fuel towards skeletal muscle that favors muscle competing postprandial fuel in circulation against adipose tissues.

• 한국습지학회지
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• 제16권2호
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• pp.193-204
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• 2014

동물의 분포는 서식지선택에 영향을 받으며, 서식지의 특성과 먹이자원은 종의 생존에 중요한 요인으로 작용한다. 본 연구는 천마산에 서식하는 쇠살모사(Gloydius ussuriensis)의 분포 패턴 특성을 파악하고자 고도, 서식지 특성, 잠재적 먹이자원인 양서류의 분포에 초점을 맞추어 수행되었다. 서식하는 고도범위에서 선호하는 서식지 타입을 알아보고자 고도를 3개의 범주(저고도, 중고도, 고고도)로 분류하였고, 서식지는 수생태계의 존재 유무에 따라 분류하였다. 쇠살모사의 경우, 고도와 서식지 타입에 따른 분포 모두 유의한 차이를 보였으며, 저고도와 물이 있는 계곡에서 주로 분포하였다. 양서류의 경우도 고도와 서식지에 따라 쇠살모사와 동일한 분포패턴을 보였다. 물이 있는 계곡의 쇠살모사와 양서류에 대한 미소서식지 분석결과는 유의한 차이가 없었다. 결과적으로 쇠살모사가 저고도에 위치한 물이 있는 계곡주변에서 대부분 분포하고 있었던 이유는 양서류의 분포가 그 원인으로 판단된다. 이러한 이유는 천마산에 서식하는 쇠살모사가 비교적 사냥하기 쉬운 먹이자원인 양서류를 선호했기 때문이라고 판단된다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2007년도 제29회 추계학술대회논문집
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• pp.23-26
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• 2007

본 연구에서는 고공 환경을 모사하기 위해 선행되어야 할 저온 환경 구축에 대한 기초 실험을 수행하였다. 열교환기를 이용하여 공기를 극저온으로 냉각 시키고, 상온의 공기를 혼합하여 온도 특성을 고찰하였다. 오리피스를 사용하여 각각의 유량을 제어할 수 있는 시스템을 구축하였으며, 열교환을 위하여 액체질소를 사용하였다. 열교환기를 통하여 냉각된 공기의 온도를 일정하게 유지시키면서 상온의 공기를 혼합시킨 결과 상온의 공기 유량이 증가함에 따라 혼합 공기의 온도도 거의 선형적으로 증가함을 확인하였다. 이에 따라 저온 환경 구축에 필요한 다양한 유량의 저온 공기를 생성할 수 있는 가능성을 확보하였다.

• International Journal of Aeronautical and Space Sciences
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• 제10권1호
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• pp.67-74
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• 2009

In general, the lunar landing stage can be divided into two distinct phases: de-orbit and descent, and the descent phase usually comprises two sub-phases: braking and approach. And many optimization problems of minimal energy are usually focused on descent phases. In these approaches, the energy of de-orbit burning is not considered. Therefore, a possible low perilune altitude can be chosen to save fuel for the descent phase. Perilune altitude is typically specified between 10 and 15km because of the mountainous lunar terrain and possible guidance errors. However, it requires more de-orbit burning energy for the lower perilune altitude. Therefore, in this paper, the perilune altitude of the intermediate orbit is also considered with optimal thrust programming for minimal energy. Furthermore, the perilune altitude and optimal thrust programming can be expressed by a function of the radius of a parking orbit by using continuation method and co-state estimator.