• 한국항공운항학회지
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• 제18권4호
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• pp.106-112
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• 2010

After a series of aircraft noise measurements conducted in Noise Sensitive Areas(NSAs) in Gangwha Island, there appeared to be no regions affected by aircraft noise of over 75 WECPNL, the legal noise level standard for aircraft operations. However, with regard to the future environment where flight operations at Incheon International Airport are likely to escalate, an INM analysis result drawn shows that the number of regions afflicted by such noise will increase in Gangwha Island. Therefore, we studied similar cases from developed countries, which are pertinent to solutions for aircraft noise abatement in the vicinity of airports and herewith provided 6 more flight operation procedures other than those 3 currently in service at Incheon International Airport.

• 한국항공운항학회지
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• 제11권1호
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• pp.27-40
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• 2003

For the flight education, it needs a lot of money. Most of people become airline transportation pilots after completing a course. Therefore it is important to select superior students who adapt themselves to flight for flying education. At present, students who have a good high school record and SAT(Scholastic Aptitude Test) are chosen, and educated at Hankuk aviation university, department of aeronautical science and flight operation. This research studies the professor's recognition of the relationship between practical flight skills and high school record, university grades, and SAT grades.. On this analysis result, there are significant differences between belonging education, completion and work experience.

• 한국항공운항학회지
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• 제20권1호
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• pp.55-65
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• 2012

An airman licensing system is central to the establishment and management of a state's airman licensing which gives official privileges to a person to perform specific activities by evaluating applicant's knowledge and proficiency. In recent decades, the level of the domestic aviation industry continues to leap forward and state's airman licensing system has also been advanced. However, accidents caused by pilot human errors are still occurring. In particular, the pilot occupations require a lot of experience and knowledge and the student pilots receiving the initial flight training have formed their own flight habits based on knowledge, skill, training methods, procedures, etc learned from the flight instructor. This paper discusses possible ways on the improvement for the domestic flight instructor rating by analyzing domestic and international rules and procedures for a flight instructor rating.

• International Journal of Aerospace System Engineering
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• 제5권1호
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• pp.9-18
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• 2018

The longitudinal flight parameters of a light airplane are estimated from flight test data by use of the output error method. The reliability of the flight test measurement is examined in engineering judgment, scatter and Cramer-Rao bound, which turns out to be satisfactory with minor defects. Estimated parameter values are validated by comparing the simulated responses with the ones from actual flight tests. The FTD(Flight Training Device) of a light airplane turns out to satisfy the qualification of FAA Level 5 FTD in longitudinal motion. All the necessary practices for generation of high-fidelity data in longitudinal motion of a light aircraft are successfully performed in this study.

• 한국항공운항학회지
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• 제18권3호
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• pp.77-83
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• 2010

"The prohibition of careless or reckless flight" is the regulation specified not only in the national air law but ICAO ANNEX and FAR. This article(item) has not been categorized properly unlike other items and the question such as why this is described as a fundamental and essential act can be answered only by the party subjected to administrative measures in case of Korea and this kind of violation is so rare that it is not easy to understand the legal meaning and the function of the term, "The prohibition of careless or reckless flight" In case of U.S where aviation cases are common, the distinction between the term "careless" or "reckless" operation depends on whether to recognize the given situation. Some incidents happened by failing to aware NOTAM, violating ATC, or T/W landing where a pilot did not recognize the violation itself are considered to be "Careless" flight. Others such as low altitude high speed flight, approximate flight, Rejecting ATC instruction where a pilot intends to or is remiss in safety are regarded as "Reckless" flight. For pilots who are required to take the highest level of care from preparing for flight to stopping engines or completely disembarking passengers from a plane, the clear understanding of the most basic concept of "careless" or "reckless" flight should be emphasized for the safe flight and it is the time for the authorities to set a standard for proper measures by definite legal interpretations.

• 전자공학회논문지SC
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• 제46권3호
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• pp.59-65
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• 2009

최근 무인기의 형태는 다양한 형태로 개발되고 있으며, 탑재 장비의 고성능 소형화를 바탕으로 무인기는 소형화되고 있다. 이러한 소형화되고 일반적인 형태가 아닌 무인기 개발에 있어, 기존의 개발방법으로는 이러한 비선형적인 요소로 인하여 정확한 모델링 및 제어기 알고리즘의 정형화하기가 어렵다. 따라서 본 논문에서는 기존이 비행체 개발 방법이 아닌, 하중 제어 개념을 적용한 Min 설계 방법의 첫 번째 단계로, 원통형 무인기에 적용하여, 수평 비행 조건과 특성 그리고 제어기 설계 알고리즘을 찾아보았다. 이러한 Min 설계 방법은 고성능 컴퓨터를 사용한 무인기 개발에 있어 실시간 시뮬레이션을 통한 비용절감과 개발기간을 단축시킬 수 있다.

• 한국전자파학회논문지
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• 제30권6호
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• pp.487-497
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• 2019

탄도미사일은 작은 레이다 단면적 및 빠른 기동 특성으로 인하여 탐지가 매우 힘들며, 또한 탄도미사일의 각 비행단계에서 탄두와 유사한 운동 변수로 기동하는 연료탱크 및 기만체의 존재로 인하여 탄두의 식별 및 요격이 매우 어렵다. 따라서 비행 단계에 따라 표적의 기동 및 미세운동을 이용한 특성벡터가 필요하며, 또한 이를 적절히 융합하여 비행단계에 상관없이 식별하는 방법이 요구된다. 본 연구에서는 탄도미사일의 비행단계에 따른 유용한 특성벡터를 소개하고, 이를 특성벡터 및 구분기 레벨에서 융합하는 효과적인 기법을 제안한다. CAD 모델들을 사용하여 예측된 레이다 신호들로 시뮬레이션을 수행한 결과, 구분기 레벨 융합을 통하여 잡음환경 내에서 비행단계에 상관없이 종말 단계로 갈수록 보다 향상된 탄두 식별이 가능하였다.

• 한국항공우주학회지
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• 제41권1호
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• pp.10-16
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• 2013

본 논문에서는 풍동 실험을 통해 취득한 소음측정 결과에서 실제 비행에 기체에서 발생되는 소음을 예측하는 과정에 대하여 다루었으며 정지된 소음원을 비행하는 것과 같은 상태로 시뮬레이션 할 수 있는 방법에 대하여 소개하고 실험을 통하여 검증하였다. 또한 국제민간항공기구(이하 ICAO)에서 규정한 절차에 따라 틸트로터 항공기 및 무인항공기의 환경소음을 평가할 수 있는 방안을 제시하였다. 제시한 평가 방안을 검증하기 위해서 풍동실험과 비행시험에 대한 소음실험 시뮬레이션 프로그램을 구성하였으며 7kg급 무인항공기를 통한 풍동 실험 및 비행 실험을 수행하였으며 풍동 실험 결과로부터 비행 상태의 소음예측이 가능하다는 것을 확인 할 수 있었다.

• 한국소음진동공학회논문집
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• 제15권12호
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• pp.1327-1331
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• 2005

This Paper addresses what amount of whole-body vibration is exposed to Korean pilots of UH60 helicopters during their mission flight. To measure the expose4 whole-body vibration, the 12-axis whole-body vibration measurement system was used. It enables the direct measurement of whole-body vibration exposed from the body contact area consisting of the feet, hip and back. The measured 12-axis vibration signals were used to evaluate the vibration comfort level experienced by the pilots of UH60 helicopters. The evaluated vibration comfort level is found to be closeto 0.74-0.79m/s, which is equivalent to the semantic scale of 'fairly uncomfortable'. To assess the health effects of whole-body vibration exposed to Korean pilots of UH60 helicopters during their mission flight, the rms-based and VDV(vibration dose value)-based evaluation schemes, recommended by ISO 2631-1:1977, were exploited in this work. The evaluated results indicate that Korean pilots cannot avoid the fatigue-decreased proficiency limit after two-hour continuous flight. The whole-body vibration level exposed from the UH60 helicopters during continuous 10-hours mission flight is found to reach to the vibration exposure limit.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2005년도 춘계학술대회논문집
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• pp.132-137
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• 2005

This paper addresses what amount of whole-body vibration is exposed to pilots of UH60 helicopters during flight. To measure the whole-body exposed from the feet and seat, the 12-axis vibration measurement system was used. It enables simultaneous measurement of vibration exposure from the body contact area of the feet, hip and back. The measured 12-axis vibration signals are exploited to the comfort level of UH60 helicopters during flight. It is shown that the evaluated ride value is close to $0.74{\sim}0.79m/s^2$ and that it is equivalent to the semantic scale of 'fairly uncomfortable'. To assess the health effects of whole-body vibration exposed to pilots of UH60 helicopters during their flight, the rms-based and VDV(vibration dose value)-based evaluation results of measured four-axis vibration signals are shown in this work. The fatigue-decreased proficiency limit, whose level is half of the exposure limit, is expected to come after the two-hour flight. The exposure limit is shown to reach after the 10-hour flight.