• 한국항공우주학회지
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• 제46권8호
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• pp.671-678
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• 2018

헬리콥터 소음예측은 저소음 헬리콥터 기술 개발에 필수적인 과정이다. 본 논문에서는 헬리콥터 통합성능해석프로그램 CAMRAD-II와 자체개발한 소음해석코드를 이용하여 소음예측 기법을 구축하였다. 또한 헬리콥터 소음 중 가장 큰 원인인 블레이드-와류 간섭 소음을 분석하여 해석기법을 검증하였다. 실제적인 소음예측을 위해 국제민간항공기구(ICAO)에서 기준으로 하고 있는 헬리콥터 소음 측정 비행조건인 Flyover, Approach 조건에 대해서 소음해석을 수행하였으며, 최종적으로 비행시험결과 와의 비교 분석을 통해 해석방법의 적합성을 확인하였다.

• International Journal of Aeronautical and Space Sciences
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• 제13권3호
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• pp.377-385
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• 2012

The Automatic Dependent Surveillance Broadcast (ADS-B) system is a key component of CNS/ATM recommended by the International Civil Aviation Organization (ICAO) as the next generation air traffic control system. ADS-B broadcasts identification, positional data, and operation information of an aircraft to other aircraft, ground vehicles and ground stations in the nearby region. This paper explores the ADS-B based trajectory prediction and the conflict detection algorithm. The multiple-model based trajectory prediction algorithm leads accurate predicted conflict probability at a future forecast time. We propose an efficient and accurate algorithm to calculate conflict probability based on approximation of the conflict zone by a set of blocks. The performance of proposed algorithms is demonstrated by a numerical simulation of two aircraft encounter scenarios.

• 한국항행학회논문지
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• 제28권3호
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• pp.375-378
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• 2024

The instrument landing system (ILS) is an international standard established by the International civil aviation organization (ICAO) as one of the landing support facilities for aircraft. This system consists of a localizer (LOC) that provides orientation information about the runway to indicate the approach direction, a glide path (GP) that indicates the appropriate approach glide slope, and three of marker beacons (MB) that indicates the distance to the runway landing edge. In this study, we predicted the received signal strength by altitude and distance for LOC signals transmitted from the ground and analyzed the difference with the signal strength measured in the actual environment. Our objective is to develop signal strength prediction technology and apply it to the real environment.

• 항공우주정책ㆍ법학회지
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• 제22권1호
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• pp.163-186
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• 2007

Charter flight in international air law has, from very beginning, not precisely defined by the International Civil Aviation Organization (lCAO) since 1947 when it came into being. By practice, the operation of charter traffic is, in its very beginning, the subject to the regulations of national rules and bilateral charter agreements (charter annex clause) within the framework of normal bilateral agreement of international air services. Taiwan had signed a series of bilateral air service agreement under the name of the Government of the Republic of China when Taiwan was recognized by the United Nations and major members of international community as the sole legal government representing China before 1971, but that situation was changed since then. Taiwan has only maintained diplomatic relations with 25 States, but maintained semi-official relations with major powers of the world. The former agreements were signed within the framework of the Vienna Convention on the Law of Treaties of 1969 while the latter agreements were signed within the framework of administrative and civil law of two countries which were not in the form of bilateral treaty signed by two sovereign States in its proper sense of international law. The legal regime of charter flights between Taiwan and Mainland China is regulated by special arrangements negotiated by delegated airlines and airlines association or private law institutions.

• 한국항행학회논문지
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• 제19권3호
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• pp.175-181
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• 2015

최근 운항경로 단축, 연료 절감, 운항시간 지연 축소, 항로 수용력 증대 등의 공역 혼잡해소 및 미래수요 대처에 대한 방안수립이 요구되어지고 있으나, 현재의 재래식 항행시설장비만으로는 한계가 있어 GNSS를 이용한 위성항법 광역보강시스템인 SBAS(satellite based augmentation system)가 고려되어지고 있다. ICAO는 2025년부터 SBAS를 활용한 항공기 운항을 권고하고 있으며, 우리나라도 이에 발맞추어 한국형 위성항법보강시스템인 KASS (Korea augmentation satellite system)를 개발 중에 있다. 본 논문에서는 KASS 개발이 완료되는 시점인 2022년 이전에 KASS 비행시험 및 검사 절차를 수립하기 위하여 SBAS 비행검사 관련 ICAO 및 FAA 규정을 분석하고 도출된 기준 항목들은 향후 KASS 비행시험 및 검사과정에 참고 될 수 있을 것으로 기대된다.

• 국토계획
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• 제53권7호
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• pp.39-48
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• 2018

The purpose of this study is to verify the stable flight conditions of drones within a limited urban area by using the ICAO(International Civil Aviation Organization) reich model which is using to evaluate civil aircraft stability. The results of the study are summarized as follows. First, in order for the drones flying stably, the horizontal safety separation distance between a drone and another should be at least 1,852M. Second, assuming that no obstacles within 1,852M of horizontal space, two drones can be fly into upper and lower spaces. However there are obstacles such as buildings, it is impossible to secure a 1,852M distance between drones. Third, sensitivity analysis point out that the separation interval($s_x$) of drone aviation has the greatest influence on the TLS(Target Level of Safety). If future research is conducted to lower the numerical values, the safety distance between a drone and another drone will be drastically reduced, allowing more detailed urban space division, and will be presented as a scientific numerical value for establishing a dedicated path for the drones.

• Journal of Positioning, Navigation, and Timing
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• 제12권4호
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• pp.349-358
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• 2023

The Satellite-Based Augmentation System (SBAS) plays a significant role in the fields of aviation and navigation: it corrects signal errors of the Global Navigation Satellite System (GNSS) and provides integrity information to facilitate precise positioning. These SBAS systems have been adopted as international standards by the International Civil Aviation Organization (ICAO). In recent SBAS system design, the Minimum Operational Performance Standards (MOPS) defined by the Radio Technical Commission for Aeronautics (RTCA) must be followed. In October 2014, South Korea embarked on the development of a Korean GPS precision position correction system, referred to as Korea Augmentation Satellite System (KASS). The goal is to achieve APV-1 Standard of Service Level (SoL) service level and acquisition of CAT-1 test operating technology. The first satellite of KASS, KASS Prototype 1, was successfully launched from the Guiana Space Centre in South America on June 23, 2020. In December 2022 and June 2023, the first and second service signals of KASS were broadcasted, and full-scale KASS correction signal broadcasting is scheduled to start at the end of 2023. The aim of this study is to analyze the precision of both the GNSS system and KASS system by comparing them. KASS is also compared with Japan's Multi-functional Satellite Augmentation System (MSAS), which is available in Korea. The final objective of this work is to validate the usefulness of KASS correction navigation in the South Korean operational environment.

• 한국항공운항학회지
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• 제27권4호
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• pp.105-113
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• 2019

The commercial pilot retirement age has continued to 65 since the International Civil Aviation Organization(ICAO) amended the recommended age limit from 60. The target of this review is to analyse whether aged pilots have an increased age-dependent risk of medical incapacitation. Medical in-flight incapacitation is actually very rare event and the demonstrated annual incapacitation rate provides an acceptable risk within the criteria known as 1% safety rule for a pilot undertaking air transport operations while some controversies exist. There is a possibility that the accident rate has decreased due to the improved skill by increasing pilot's age. At the decision of flight or not for elderly airline pilot the interacting factors of personal health status, piloting experience and new flight environments should be considered to define job limit criteria than mere the age. Results of a survey led by airline pilot association in Korea shows 65% of airline pilots are willing to fly without any age limit and 87% agreed that age limit is worthy to extend beyond current standard on the basis of medical examinations. Only 11% agreed to maintain current age limit.

• 항공우주시스템공학회지
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• 제14권spc호
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• pp.39-48
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• 2020

본 논문에서는 풍동 실험을 통해 측정한 소음 결과를 활용하여 실제 비행하는 기체에서 발생되는 소음수준을 예측하고 비행시험을 통해 검증하는 과정을 다루었다. 항공기의 환경소음 평가를 위해서는 일반적으로 국제민간항공기구(이하 ICAO)에서 규정한 절차에 따라 소음시험 및 평가를 수행하게 된다. 본 논문에서는 고정익 및 회전익(멀티콥터)의 특징을 모두 가지고 있는 복합형 기체에 적용이 가능한 환경 소음평가 방안과 실험을 통해 검증한 결과를 제시하였다. 고정익과 회전익 소형 무인기를 활용하여 풍동실험에서 측정한 소음시험 결과를 실제 비행 시험결과로 시뮬레이션 하는 과정을 제시하였다. 또한, ICAO에서 제시하는 비행 운용조건 및 소음 측정 방법을 고려하여 풍동실험을 통한 결과와 실 기체 비행시험을 모두 수행하여 항공기 소음인증을 위한 실효감각소음레벨(EPNL)을 예측 및 고찰하였다.

• 한국항행학회논문지
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• 제15권4호
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• pp.510-516
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• 2011

위성항법시스템(GNSS)을 민간항공 분야에 활용하기 위해서는 국제민간항공기구(ICAO)가 정한 비행단계별 정확성(Accuracy), 무결성(integrity), 연속성(continuity), 가용성(availability) 성능요구조건을 만족시켜야 한다. 사용자의 무결성을 확보하기 위해서는 사용자의 보호 수준을 크게 잡아야 하고 가용성을 향상시키기 위해서는 보호수준이 작을수록 좋다. 따라서 주어진 항행요구조건을 만족하기 위해서는 사용자의 무결성을 확보하면서 보호수준을 최대한 작게 잡아야 한다. 본 논문에서는 한국형 광역보정시스템 테스트베드 중앙처리국 모듈의 현재까지 진행 상황에 대해서 설명하고 현재 사용되고 있는 무결성 관련 알고리듬을 적용하였을 때 사용자의 무결성 및 가용성 성능에 대한 예측을 수행하였다. 또한 항법위성의 궤도 및 시계오차에 대한 공분산 행렬을 사용자 무결성 감시에 적용하였을 때의 가용성 향상 정도를 시뮬레이션을 통해 예측하도록 한다.