• 한국항행학회논문지
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• 제17권3호
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• pp.279-284
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• 2013

운항의 여러 단계 중 착륙단계에서 조종사들이 많은 부담을 느낀다. 이는 조종사들이 항공기 속도를 줄이고 접지하여 완전히 정지하는 동안 착륙안전에 영향을 미치는 여러 요소가 있기 때문이다. 만일 착륙하는데 활주로길이가 충분하다면 부담이 적을 수도 있다. 그러나 항상 그런 경우만 있는 것은 아니다. 따라서 착륙성능이 제한범위 내에 있는지 아닌지를 확인할 필요가 있다. 필요착륙거리는 시험비행 조종사에 의해 실증되어진 실제착륙거리에다가 항공사의 평균적인 조종사들을 위한 여유분을 포함한 것이다. FAR의 AFM(항공기 비행규정) 인가는 건조 및 습윤 활주로에서 수동착륙을 기반으로 한다. 기타 다른 활주로 조건에서는 인가가 필요하지 않다. JAR에서는 빙설/윤활활주로에서도 정해진 여유분을 포함시키도록 규정하고 있다. 자동착륙은 인가사항이 아니므로 실제착륙거리만 제공된다. 본 논문에서는 각 활주로 조건에서 포함된 거리 여유분을 분석하고자 한다. 또한 특정한 활주로 조건에서 여유분이 규정되어 있지 않은 경우 대안을 제시하고자 한다.

• 한국항공우주학회지
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• 제41권6호
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• pp.458-464
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• 2013

본 논문에서는 무인 항공기의 활주로 자동 접근 알고리즘에 대해 기술하였다. 본 연구에서 자동 접근의 주요 목적은 야간에 항공기의 안전한 착륙을 돕기 위함이다. 자동 접근 기능을 사용하게 되면 항공기가 어느 위치에 있던 초기 위치를 기준으로 경로 명령이 생성된다. 경로 명령은 최단거리를 가지는 원호-직선-원호로 구성되어있다. 경로 명령을 통해 생성된 경로를 따라 이동한 다음 활주로에 접근하도록 알고리즘을 설계하였다. 항공기의 다양한 초기 위치에 대한 경로 생성 알고리즘의 시뮬레이션을 통해 1차 검증을 하였으며 이를 기반으로 실제 비행시험을 수행하여 본 연구에서 제안한 알고리즘의 타당성을 실증적으로 검증하였다.

• 한국운동역학회지
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• 제22권1호
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• pp.25-34
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• 2012

The purpose of this study was to determine the effects of landing height on the lower extremity during a counter movement jump. Fourteen healthy male subjects (age: $27.00{\pm}2.94$ yr, height: $179.07{\pm}5.03$ cm, weight: $78.79{\pm}6.70$ kg) participated in this study. Each subject randomly performed three single-leg jumps after s single-leg drop landing (counter movement jump) on a force platform from a 20 cm and 30 cm platform. Paired t-test (SPSS 18.0; SPSS Inc., Chicago, IL) was performed to determine the difference in kinematics and kinetics according to the height. All significance levels were set at p<.05. The results were as follows. First, ankle and knee joint angles in the sagittal plane increased in response to increasing landing height. Second, ankle and knee joint angles in the frontal plane increased in response to increasing landing height. Third, there were no significant differences in the moment of each segment in the sagittal plane for the jumping height increment. Fourth, ankle eversion moment and knee valgus moment decreased but hip abduction moment increased for the jumping height increment. Fifth, Ankle and knee joint powers increased. In percentage contribution, the ankle joint increased but the knee and hip joints decreased at a greater height. Lastly, as jumping height increased, the power generation at the ankle joint increased. Our findings indicate that the height increment affect on the landing mechanism the might augment loads at the ankle and knee joints.

• 한국항행학회논문지
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• 제19권5호
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• pp.403-410
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• 2015

ADS-B는 레이더에 비하여 높은 정확도와 빠른 갱신 주기를 제공하여, 레이더를 대체하거나 보완할 수 있는 기술이다. 최근 증가하는 항공교통량과 이에 따른 정확한 감시의 요구에 의하여 ADS-B가 실제 항공기 운영에 적용되고 있다. 본 논문은 항공기가 운항 중 상시 송신하는 ADS-B 신호를 활용한 공한 인근 지역에서 정밀 감시가 가능한지 확인하기 위한 자료 수집과 일부 데이터에 대한 분석을 수행하였다. 이를 위하여 정밀계기 착륙 접근하는 항공기의 ADS-B 항적을 수집하고, 최종접근 구간에서 항적의 분포 특성에 관한 분석을 수행하였다. 분석결과 ADS-B 항적은 활주로 중심선 연장선에 대하여 평균 이격 거리 -0.04 m, 표준편차 6.71 m이고, 또한 비교적 정확한 감시정보의 제공이 가능함을 확인하였다.

• 한국운동역학회지
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• 제22권4호
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• pp.395-404
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• 2012

This study was to perform the kinetic analysis of tucked backward salto on the balance beam. Eight women's gymnastics players(age: $15.88{\pm}2.45yrs$, career: $6.38{\pm}0.52yrs$, height: $152.38{\pm}7.35cm$, weight: $44.25{\pm}7.54kg$) of the I-region participated in this study. The kinematic variables were analyzed response time of motion, angle, velocity, acceleration and the kinetic variables were analyzed ground reaction force(GRF) of motion. For measure and analysis of kinematic and kinetic variables of this study, used to synchronized to 6 Eagle camera and 1 force plate, used to the Cortex(Ver. 1.0) for analyzed of variables. The results were as follows; To the kinematic variables of tucked backward salto on the balance beam, a time appeared longer landing than air rotation, changes of angle regulated segment of body smaller moment of inertia when air rotation, larger moment of inertia when releasing and landing. A velocity appeared fast motion when releasing and air rotation of body, but appeared more decelerations from landing and acceleration showed to be tended to velocity. A GRF appears jump more than twice the weight at the moment that showed the power of motion to all subject.

• 한국항행학회논문지
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• 제27권6호
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• pp.888-896
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• 2023

항공기 착륙 시에는 정해진 절차에 따라 접근이 이루어진 다음, 활주로 중심선과 정렬하여 착륙하게 된다. 하지만 공항의 상황, 주변 항공기의 상황, 또는 관제사의 지시 등에 따라 빈번한 레이더 벡터링이 일어나기 때문에, 교통 흐름을 파악하거나, 비행 안전성을 파악하기 위해서는 항공기의 접근 패턴을 인지할 필요가 있다. 또한 최종 접근 시 활주로 중심선과 정렬하는 과정에서 과이탈이 발생하는 경우가 있는 데, 이는 이후 불안정 접근 등과 같이 보다 위험한 상황을 초래할 수 있다. 본 논문에서는 클러스터링 기법을 이용하여 접근 구간에서의 항공기 궤적들의 패턴을 추출하였다. GMM (Gaussian Mixture Model)을 이용하여 김해공항 접근 항공기 궤적에 대한 클러스터링을 진행하였으며, 2019년 1년간 김해공항으로 착륙한 항공기의 데이터를 이용하였다. 클러스터 별 centroid 값을 이용하여, 총 86개의 접근 궤적 패턴을 추출하였다. 그 후 각 클러스터 내 항공기 중 최종 접근시 과이탈하는 항공기를 탐지하여 확률 분포를 계산하였다.

• 한국의류학회지
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• 제32권7호
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• pp.1023-1033
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• 2008

The purpose of this study was to segment home-shopper market by using the demographic characteristics. This study enables a better unders landing of home-shoppers and improving the strategy of marketing. The specific objects of this study are as follow: First, it was to exam market segmentations by demographic factors using mixture model. Second, it was to exam shopping orientations of fashion merchandise according to segmentation groups. The data was collected from 637 subjects who had used the home shopping more than one time in a year. The data was analysised through frequencies, factor analysis, ANOVA, Duncan's mutiple range tests with SPSS 12.0 and Mixture model. The results of data are as follows: 1. The result of market segmentation as demographic factor using Mixture model was extracted to 4 market segments called 20's/ unmarried stage, 30's/ children bearing & rearing stage, 40's/ families with children's education stage, 50's/ aging stage. 2. Shopping orientations were extracted to 5 factors called a pleasure oriented, convenience oriented, off-line oriented, human oriented, thrift oriented.

• 한국항공우주학회지
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• 제32권5호
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• pp.1-9
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• 2004

수직이착륙과 고속수평비행이 기능한 스마트 무인기 개발의 일환으로 초기개념설계용 성능예측 프로그램을 작성하였다. 스마트 무인기가 요구하는 설계조건을 기반으로 각 임무 단계 수행과정에서의 연료소모중량을 반복계산하여 전체 중량을 예측하고, 동시에 무인기의 주요형상변수, 추진성능, 수직이착륙성능, 수평비행성능 등의 계산을 통해 성능예측 및 설계요구조건 만족여부 판단, 경향성 분석을 수행할 수 있다. 동 프로그램은 수직이착륙 무인항공기 비행체의 초기개념설계단계에서 비행체의 경향성 분석, 비행성능 예측 및 설계 요구조건 검증 등을 손쉽고 간편하게 수행 할 수 있는 도구도서 사용할 수 있다.

• 무역상무연구
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• 제78권
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• pp.1-29
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• 2018

This article demonstrates that both the Warsaw Convention Systemand the Montreal Convention are not designed for multimodal transport, let alone for "Door to Door" transport. The polemic directed against the "Door to Door" application of the Warsaw Convention systemand the Montreal Convention is predominantly driven by the text and the drafting philosophy of the said Contentions that since 1929 support unimodalism-with the rule that "the period of the carriage by air does not expend to any carriage by land, by sea or by inland waterway performed outside an airport" playing a profound role in restricting their multimodal aspirations. The drafters of the Montreal Convention were more adventurous than their predecessors with respect to the boundaries of the Montreal Convention. They amended Art. 18(3) by removing the phrase "whether in an aerodrome or on board an aircraft, or, in the case of landing outside an aerodrome, in any place whatsoever", however, they retained the first sentence of Art. 18(4). The deletion of the airport limitation fromArt. 18(3) creates its own paradox. The carrier can be held liable under the Montreal Convention for the loss or damage to cargo while it is in its charge in a warehouse outside an airport. Yet, damage or loss of the same cargo that occurs during its surface transportation to the aforementioned warehouse and vice versa is not covered by the Montreal Convention fromthe moment the cargo crosses the airport's perimeter. Surely, this result could not have been the intention of its drafters: it certainly does not make any commercial sense. I think that a better solution to the paradox is to apply the "functional interpretation" of the term"airport". This would retain the integrity of the text of the Montreal Convention, make sense of the change in the wording of Art. 18(3), and nevertheless retain the Convention's unimodal philosophy. English courts so far remain loyal to the judgment of the Court of Appeal in Quantum, which constitutes bad news for the supporters of the multimodal scope of the Montreal Convention. According the US cases, any losses occurring during Door to Door transportation under an air waybill which involves a dominant air segment are subject to the international air law conventions. Any domestic rules that might be applicable to the road segment are blatantly overlooked. Undoubtedly, the approach of the US makes commercial. But this policy decision by arguing that the intention of the drafters of the Warsaw Convention was to cover Door to Door transportation is mistaken. Any expansion to multimodal transport would require an amendment to the Montreal Convention, Arts 18 and 38, one that is not in the plans for the foreseeable future. Yet there is no doubt that air carriers and freight forwarders will continue to push hard for such expansion, especially in the USA, where courts are more accommodating.

• 한국운동역학회지
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• 제22권3호
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• pp.269-276
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• 2012

The purpose of This study's aim is to examine the difference in the changes of body segment movement, variables for ball quality, and carry at golf driver swing according to the ball quality using comparative analysis. Regarding the impact variables according to the ball quality using the track man and carry, club speed was the fastest at draw shot, ball speed was the fastest at straight shot, and smash factor was the lowest at draw shot. About the vertical launch angle, the fade shot showed the highest launch angle while the max height of the ground and ball was the highest at fade shot. And carry was the longest at draw shot. For the flight time, it was the longest at draw shot. The landing angle was the largest at fade shot. About the club head position change and trajectory, at the overall event point, the fade shot drew a more outer trajectory at the point of the follow through(E6) than the straight or draw shot. Regarding the angular speed of shoulder rotation, at the overall event point, the fade shot showed the greatest angular speed change in the follow through(E6). Also, about the angular speed of pelvic rotation, at the overall event point, the draw shot showed the greatest angular speed change at the point of down swing(E4). Concerning the stance angle change, both straight and fade shots were open as the concept of open stance whereas the draw shot was close as that of close stance. Regarding the previous study, the most important factor of deciding Ball Quality is the club face angle's open and close state at Impact. In short, the Ball Quality and carry were decided by this factor.