• 한국항공운항학회지
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• 제13권3호
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• pp.73-84
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• 2005

Hanseo University's Tae-an Airfield was opened in July, 2005 for aeronautical education such as aircraft flight, air traffic control, avionics, etc., and will play an important part as a base for local economic and industrial developments. On the contrary, the aircraft noise from the airfield will give an impact against the vicinity of the airfield and become a big issue which the airfield authority has to solve. The aim of this study is to analyse the aircraft noise contour in vicinity of the airfield and to make understand the people around the airfield how much the aircraft noise will have an effect on. For the prediction of the aircraft noise in the local area, this study showed the method to assess the aircraft noise in the developed countries for aviation, and the result to compute WECPNL by INM 6.1 after encoding the various data including environmental input data, tract, and profile. The major results of the study can be summarized as follows ; While the area with influence contour of noise from 75 to 80 WECPNL is 0.555$km^2$, the area from 80 to 85 is 0.343$km^2$, and the area with influence contour of noise over 85 WECPNL is 0.163$km^2$. In addition, there are 4 houses in the contour over 85 WECPNL and the inhabitants(10 people) in this area will have effect from the noise. Therefore Tae-an airfeild authority is preparing the noise-prevention method or noise abatement program. Finally, according to the noise contour, it is one of the best way of decreasing the effect of aircraft noise that 33 runway is assigned as calm-wind runway because there is no resident in the area around 15 threshold.

• 한국항공운항학회지
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• 제21권3호
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• pp.9-14
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• 2013

Continuous airworthiness system is comprised of regulations and procedures to assure the safety and reliability through the total stage of development, certification and operation of aircraft. The purpose of this system is not only to provide the guidelines that should be kept by manufacturers and operators, but also to evaluate the maintenance capability in every activity of safety related procedures. During the development process of the mid and large size aircraft, operational experience should be reflected systematically for a safer and more reliable product by using the meaningful data base from operation. The relationship of safety roles between manufacturer and operator is mutually complementary, and the roles of each function have an influence to the next step. Overall structure of the procedure contains the concept of continuous analysis and feedback to achieve highest degree of safety and reliability during the entire life of aircraft. Finally, this paper describes how the feedback is made and used for aircraft design from operational experience under the continuous analysis and surveillance system.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 1995년도 제4회 학술강연회논문집
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• pp.71-81
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• 1995

The Propulsion System Integration can be defined as the optimization technology of combining the propulsion system components with the airframe to achieve the overall aircraft misson performance goals. The disposition of propulsion system components on engine compartment enveloped by front fuselage and fire bulkhead is very restricted because of the interference with nose L/G and engine mountig strut. The design of components depends on the traditional technical data base. The engine satisfying a customer's ROC was selected among worldwide existing engines by the comparision studies of performance analysis with enigine installed effect, future growth potential, ILS, and application to aircrafts, etc. The ground test of the propulsion system integration was performed in the test cell and on the aircraft to assure the function of the components. The flight test was performed to confirm complying the performance requirements.

• 한국항공운항학회지
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• 제20권2호
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• pp.1-6
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• 2012

Four dimensional(4-D) trajectory modeling is conducted based on flight plan. The flight plan is divided into several segments which represent certain operating flight modes. Thrust, drag and fuel consumption rate of an aircraft are calculated using BADA provided by Eurocontrol. The trajectory is modeled with the rate of climb/descent calculated with Total-Energy Equation. The simulation results with a typical aircraft and its flight plan indicate that the trajectory modeled corresponds well with the suggested flight plan. The performance profiles including total endurance time and time history for speed, thrust, drag and fuel consumption were also appropriately generated.

• 디지털산업정보학회논문지
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• 제7권3호
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• pp.115-121
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• 2011

The flight information visualization of the aircraft is the system which is widely used to the threat against low altitude tasks and terrain altitude. But, it is difficult to implement the system because of restrictions that GPS data and huge geographic information should be stored. In this paper, it proposes economic DMM (Digital Moving Map) system for flight information visualization from open-source-base. First, the flight information is transferred from X-Plane through UDP and then demonstrated on the DMM system. In the proposed DMM system, flight information is visualized on the map information downloaded from an ArcGIS Map server using the mapping data between the present altitude of the aircraft and the terrain altitude. The result of this paper could be used an economic tool in the field of flight information visualization and the game algorithm research.

• 한국컴퓨터정보학회논문지
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• 제15권12호
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• pp.181-188
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• 2010

본 논문은 수집된 항공기의 상황 자료를 이용하여 웹 기반의 구글 어스와 OpenGL을 이용한 3차원 시각화을 통하여 항공기의 올바른 상황인식과 상태정보를 지원하는 시스템을 제안한다. 기존에 제안된 시스템은 방대한 지형 자료와 지도 및 위성사진을 연동하여 표현함으로 속도 저하 및 한정된 지도 정보만을 가시화하는 문제점을 가진다. 제안하는 시스템은 개방된 구글 어스의 Open API을 이용하여 최소한의 비행 정보만으로 실시간 상황인식을 위한 경제적이고 전역적인 시각화 도구를 지원한다. 또한 사용자의시각적 편리성을 위하여 다중 위치 정보를 볼 수 있는 확장 뷰를 제공한다. 본 연구결과는 웹 환경에서 항공기의 상황인식을 지원하는 시스템으로 이용될 수 있는 가능성을 보인다.

• 한국항공우주학회지
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• 제44권5호
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• pp.423-430
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• 2016

최근 국가공역 내 유 무인항공기 혼합운용 시 충돌 감지 및 회피, 통신두절 등의 다양한 문제가 예상된다. 따라서 본 연구에서는 EUROCONTROL의 BADA와 NASA의 성능 데이터를 기반으로 유인기와 무인기 혼합운용 및 ATC/ATM 시뮬레이션을 동시에 수행할 수 있도록 필요한 환경 구축과 동적 모델링을 수행하였다. 또한 구성한 모델의 검증을 위하여 6-DOF 비행모델과 세그먼트별 동일한 입력값으로 시뮬레이션을 수행하고, RMSE결과 비교를 통해 구성한 모델의 적합함을 확인하였다.

• 한국항행학회논문지
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• 제21권3호
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• pp.264-271
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• 2017

본 논문에서는 입력된 비행계획을 바탕으로 4차원 궤적을 생성하고, 이 궤적정보를 기반으로 항공기 운동을 나타내는 시뮬레이션 모델을 개발하였다. 4차원 궤적은 BADA에서 제공하는 항공기 성능 계수와 Total Energy Model 및 베지에 곡선을 활용하여 모델링 하였으며, CTA (cntrolled tme of arival) 및 속도를 기준으로 하는 두 가지 항공기 제어 방식을 제안하였다. 시뮬레이션 결과 비행시간 및 경로에 대하여 정의된 궤적과 거의 일치하였으며, 바람 조건에 따른 각 제어 방식 별 차이점을 도출하였다. 본 연구에서 개발된 시뮬레이션 모델을 기반으로, 다양한 항공교통관리 분야 연구에 활용할 수 있을 것으로 기대된다. 향후 연구로 실제 항공기가 운항한 경로와 베지에 곡선간의 차이를 줄이기 위해 최적화 기법을 도입할 필요가 있으며, 이를 통해 개발된 시뮬레이션의 활용도를 높일 수 있다.

• 한국IT서비스학회지
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• 제22권3호
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• pp.85-100
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• 2023

The development of Airside Vehicle Control System(AVCS) at Gimpo Airport aims to reduce ground safety accidents in movement area and improve airport operation efficiency and safety management service quality. The vehicle is controlled by a brake controller RTK-antenna and On-Board Diagonostics(OBD) module. Location data is transmitted to a nearby communication base station through a Wi-Fi router and the base station is connected to the AVCS by an optical cable to transmit location data from each vehicle. The vehicle position is precisely corrected to display information using the system. The system allows airport operators to view registered information on aircraft and vehicles and monitor their locations speeds and directions in real time. When a vehicle approaches a dangerous area alarm warnings and remote brake control are possible to prevent accidents caused by carelessness of the driver in advance.

• 한국측량학회:학술대회논문집
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• 한국측량학회 2010년 춘계학술발표회 논문집
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• pp.257-258
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• 2010

최근 넓은 지역에 대해 신속하게 3차원 위치좌표 데이터를 취득하기 위하여 항공레이저 스캐닝 시스템에 의해 취득된 데이터가 활용되고 있다. 현재 작업규정에 따르면 GPS 기준국과 항공기 GPS 거리가 반경 30km 이내로 정해져 있다. 본 연구에서는 항공라이다측량을 수행하는 데 있어 국토지리 정보원에서 운영중인 GPS상시관측소를 이용한 데이터와 비교하고자 한다.