• 대한임베디드공학회논문지
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• 제9권1호
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• pp.11-16
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• 2014

When it comes to develop flight simulator, HAT (Height Above Terrain) is required to provide altitude information to the pilot who learns how to control an airplane in landing and takeoff situation. However, there might be inconsistent problem between real terrain and simulation information since current implementation of HAT simply depends on center of gravity point on the airplane. To overcome mentioned problem, in this paper, we propose how to obtain more accurate altitude information than existing scheme by making use of HAT and HOT (Height Of Terrain) information of landing equipments according to movement of the airplane. Moreover, we demonstrate the accuracy of the proposed scheme through new flight simulator developed through OSG(OpenSceneGraph) by taking example of terrain information for domestic airport.

• 한국컴퓨터정보학회논문지
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• 제15권10호
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• pp.79-86
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• 2010

본 논문은 항공기의 비행정보를 효과적으로 시각화하기 위하여 Google Earth를 이용한 시스템 구현에 대해 기술한다. 이 시스템은 Google Earth 에서 제공하는 상세한 위성 영상 정보를 이용하기 위하여 COM API 를 이용하였다. 제안하는 시스템은 항공기의 다양한 장치에서 얻어진 비행정보를 OpenGL을 이용하여 각종 계기판에 표시하고 실제 비행모습을 가시화하기 위하여 Google Earth Map에 연동하여 표시하였다. 본 연구결과는 비행평가 및 개선에 이용될 수 있고 향후, 비행소프트웨어 개발에 적용될 수 있다.

• 한국항공우주학회지
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• 제49권6호
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• pp.473-480
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• 2021

소형 무인비행체 드론의 비행제어기(Flight Controller) 소프트웨어로 널리 사용되고 있는 오픈소스(Open Source)에 대한 정적분석(Static Analysis)을 통해 소프트웨어 품질의 문제점을 분석하고 개선 방안을 제시한다. 소프트웨어 품질 기준으로는 국제적으로 널리 적용되고 있는 MISRA 코딩 규칙을 선정하였으며, 정적분석 도구는 국제 도구인증(Tool Certification)을 받아 항공분야 뿐만 아니라 안전성(Safety)이 요구되는 자동차, 철도, 원자력, 의료 등 모든 산업에서 활용되고 있는 LDRA Tool을 사용하였다. 오픈소스 모듈의 구조, 사용 데이터 분석, 코딩 규칙 준수, 품질 지표(복잡도 및 시험성) 등 소프트웨어의 품질 전반에서 안전성을 위협하는 문제점들을 발견하였으며, 이에 대한 개선 방안을 제시하였다.

• 한국항공우주학회지
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• 제48권12호
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• pp.997-1004
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• 2020

Synchropter는 서로 경사진 한 쌍의 회전날개가 동조 교차 회전하는 회전익 항공기의 일종으로 동축반전 헬리콥터와 마찬가지로 꼬리 회전날개를 제거할 수 있어서 효율적이며 간결한 형태의 비행체 구성이 가능하다. 드론 체계로서의 적합성을 검토하기 위하여 소형 Synchropter를 설계, 제작하여 비행시험을 수행하였다. 설계한 Synchropter는 로터 직경이 1.4m이며 중량이 7kg인 소형비행체로서 효율적으로 비행 특성을 확인하기 위하여 상용부품 기반으로 제작하였다. 비행 제어 시스템은 Open Architecture인 Pixhawk를 기반으로 구성하였으며, Sychropter 제어법칙을 PX4 펌웨어에 탑재할 수 있도록 개발하였다. 정성적 비행시험을 통해 Synchropter의 비행 특성을 분석하였으며, 분석 결과, 드론 체계로서의 활용 가능성을 파악할 수 있었다.

• 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.

• 대한임베디드공학회논문지
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• 제10권2호
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• pp.73-79
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• 2015

Dynamic culling scheme is usually implemented to handle overhead caused by rendering the massive large-scale terrain data in flight simulator. However, existing culling scheme without considering altitude is not suitable for flight simulator due to additional computational overhead. To solve this problem, in this paper, we propose hybrid approach by applying two dynamic culling schemes depending on altitude. In addition, we remove unnessary computational overhead by creating different z-map resolution when aircraft changes its altitude. The proposed scheme is implemented with open graphic library and tested with real terrain data. Through the experimental results, we can recognize the improved rendering speed about 8 to 73 percents as compared to existing scheme.

• 한국직업건강간호학회지
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• 제27권1호
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• pp.25-35
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• 2018

Purpose: The purpose of this study was to figure out emotional labor, healthy lifestyle, needs for health services of flight attendants and the relationships among needs for health services according to various characteristics of flight attendants. Methods: The participants of this study were 140 flight attendants who work on major and low cost airlines. Data were collected through a questionnaire from 2017 .Jan.~2017. Feb. Data were subsequently analyzed using the SPSS 21 Program. Results: The score of emotional labor was 3.76 surface acting was 3.75 and deep acting was 3.77. The average of healthy lifestyle was 2.41, and the highest was 3.13 of personal relationship and the lowest was 1.91 of eating habits. There is a positive correlation between emotional labor-deep acting and healthy lifestyle. Flight attendants demand health services for physical exercise, stress and emotional labor management, healthy eating habits, emergency treatment, prevention of fatigue, cancer screening, sexual harassment prevention, sex education and etc. Conclusion: These results show that flight attendants need to various interventions for improving healthy lifestyle and reducing emotional labor. It is necessary to develop customized health promotion program suited to their job and general characteristics.

• 한국항공운항학회지
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• 제28권1호
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• pp.59-65
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• 2020

This paper presents comparative results of configuration modeling and aerodynamic analysis to single-engine airplanes such as C-172, SR-20, and DA40NG. The software OpenVSP was used as an airplane configuration modeling tool. OpenVSP can provide the fastest method to get three-dimensional aircraft configuration from given basic data and drawings of aircraft. Parametric design input in OpenVSP, from given aircraft geometric parameters, was applied to small airplanes mentioned. New aircraft models in this study were reversely designed to coincide with the publicly obtained dimensions of the original aircraft. The basic aerodynamic analysis of newly designed modeling aircraft was performed by the vortex lattice method. Results are shown that the similarity of aerodynamic data obtained except for the lack of DA40NG. In conclusion, the modeling process applied to this work is valuable to obtain conceptual design insight in the reverse design from the small airplanes currently in use for flight training.

• 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.

• 한국컴퓨터정보학회논문지
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• 제23권8호
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• pp.17-23
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• 2018

In this paper, we implemented a flight posture simulator that intuitively understands aircraft flight posture and visualizes the principle of motion. The proposed system operates the 6 - axis motion platform according to the change of the navigation information and transmits the flight attitude to the simulator using the gyro sensor. A gyro sensor and an acceleration sensor are used together to analyze the attitude of the aircraft. The reason is that the gyro sensor has a cumulative error in the integration process. And the accelerometer sensor was compensated by using the complementary filter because noise was serious due to short term vibration. Using the compensated sensor information, the motion platform is operated by calculating the angle to be transmitted to the 6-axis motor. And visualization result is implemented using OpenGL. The results of this study can be used as teaching materials for students related to aviation in the future.