• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.49 no.12
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• pp.997-1010
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• 2021

This study collected and analyzed flight data of SpaceX's Falcon 9 launch vehicle. All missions were classified by orbital types, such as Polar, SSO, ISS, LEO and GTO missions. In characteristic maneuvers of main engine cutoff, boostback, reentry and landing burn at each stage of 1st stage launch vehicle, changes of the physical parameters like speed, altitude, dynamic pressure and acceleration were investigated. The guidelines derived from detailed maneuver analysis were suggested, which can be used as design and evaluation references for developing reusable launch vehicle.

• Proceedings of the Korean Society of Computer Information Conference
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• 2023.07a
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• pp.95-97
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• 2023

본 논문에서는 임베디드 기반의 다양한 센서를 활용한 드론의 비행기록장치 시스템 개발에 대한 새로운 아이디어를 제시한다. 이 시스템은 오픈소스 기반의 개발 보드인 라즈베리파이를 중심으로, 온도, 습도, 조도, 미세먼지 센서, 이산화탄소, 일산화탄소, 산소, 이산화질소, 아황산가스, 메탄가스, GPS, 고도 측정, IR 카메라, 카메라 모듈 센서 등 다양한 센서를 탑재하여 구성한다. 기존 드론은 주로 방역 및 방제 활동에 활용되었으나, 그 활동의 효과를 정밀하게 측정하고 분석하는 데에는 한계가 있었다. 그러나 이 논문에서 제안하는 임베디드 기반의 센서 구성은 이러한 한계를 극복할 수 있을 것으로 기대된다.

• The Magazine of the IEIE
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• v.29 no.11
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• pp.1369-1377
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• 2002

항공기 운용기술이 점차 항공전자 부품에 의존하는 수준이 높아지고 있으며 항공전자부품은 저전력 소모의 기술로 변천하여 외부의 전자장 환경에 취약성이 증대되고 있다. 또한 항공기 기체구조를 형성하는 부분도 일정부분 알루미늄에서 복합소재로 대체됨에 따라 외부 전자장 환경에 취약성 요인이 되고 있다. 따라서 고강도 전자장 환경에서 항공기의 지속적인 안전 비행과 착륙에 대한 대책이 요구되고 있다. 이러한 기술의 변모에 따라 고강도 전자장 환경에 대비한 감항기준이 제정되고 있으며 이에 따른 감항인증 절차도 제정이 되고 있다. 개발 항공기는 항공기의 제작 수준에 맞는 인증 절차를 밟아야 하며 이러한 인증의 수행은 항공기 개발 경험과 신기술에 맞는 인증절차의 개발이 병행되어야 한다.

• Bulletin of the Korean Space Science Society
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• 2002.10a
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• pp.43.2-43
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• 2002

• Bulletin of the Korean Space Science Society
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• 2003.05b
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• pp.34-34
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• 2003

• Journal of the Korean Academy of Child and Adolescent Psychiatry
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• v.16 no.2
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• pp.261-269
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• 2005

Objects : We performed this study to investigate anger, anger coping, stress response, grade differences and gender differences in delinquent adolescents who were released with warning by police. Methods The subjects consisted of 285 delinquent adolescents who participated in the intervention program for preventing delinquency and 391 school students (male : 377, female : 299/middle school : 346, high school 330) in Seoul. STAXI-K and IES were used. Results : 1) The delinquent adolescent group had the higher scores of 'state anger', 'trait anger', 'total anger' than the student group. But the delinquent adolescent group had the lower scores of 'anger in', 'anger control' and 'stress response' than the student group. 2) The male delinquent adolescent group had the higher scores of 'anger control', 'stress response' than the female delinquent adolescent group. But there was no significant difference in anger. 3) The high school delinquent adolescent group had the higher scores of 'trait anger', 'anger control' than the middle school delinquent adolescent group. The high school adolescent group had the higher scores of 'stress response' than the middle school adolescent group. Conclusion : In anger, anger coping and stress response, the normal student group were different form the adolescent group who were released with warning by police committed. According to the grade and gender, differences were reported in this study. These characteristics can be more easily and more effectively applied to programs for the adolescent group who were released with warning by police committed.

• Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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• 2016.05a
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• pp.487-489
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• 2016

In this paper, quad copter provides a method for preventing the possibility of accident in the air during a formation flight. The existing studies had a few studies upon the falls because quad copter formation flight was generally implemented indoors. Therefore, in this paper, we provide a self-diagnosis system to prevent a secondary accident for mismatching the Proportional-Integral-Derivative(PID) and detecting an abnormal communication modules each others in formation flying system. Scheme to be proposed, a system is that when one of the node meets a problem, the header node is sending the information of the current state to the server in the first and making a diagnosis itself in order to avoid the problems caused by dropping from the air. Therefore, if the difference between PID value of header node and slave node is greater than specified values or if it detects a defective sensors and communication modules, the proposed system is set to provide for moving toward a safe place. As a result, we expect that this proposed system is possible to minimize additional incidents by self adjusting the height through a self-diagnosis discovering flawed the acceleration sensor, gyro sensor and various attached sensors.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.30 no.8
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• pp.148-155
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• 2002

A study on the installation angle of solar panels is conducted as a conceptual study on solar-RFC(regenerative fuel cell) system for stratospheric airships. The airship heads for the west in winter days and the east in summer days according to wind directions. Considering this, it is found that when the solar panel is installed with the center angle of 30 degree the energy output of solar panels is maximized on winter solstice and satisfies the required energy of summer days as well. Although with the optimized solar panel installation angle, efficiency of the regenerative power system needs be improved to 47% to provide required energy of a 170m-long airship. And the required amount of efficiency improvement decreases as the airship size increases.

• Journal of Internet Computing and Services
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• v.15 no.1
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• pp.1-17
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• 2014

Flight software operated on the on-board computers in the satellite has requirements such as real-time, high reliability. These requirements make dependency between the flight software and operating environments. Further, whenever a new system is built, such problem drives that all flight software are redeveloped. Thus, the dependency problem between them should be solved. And the problem can be resolved by improving the portability of the flight software. In order to improve the portability it is required to minimize the porting cost. In this paper, we classify the portability with the portability achieving methods. Using the classified portability, we propose a platform architecture that is based on the IMA concept and provides various portability capabilities. The proposed architecture enables us to solve the problem about the development of the flight software.

• Journal of Advanced Navigation Technology
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• v.11 no.2
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• pp.137-145
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• 2007

The flight test of ADS-B is to demonstrate operational benefits to air traffic controllers and pilots when other aircraft data including the aiming altitude is displayed on CDTI. Additionally, This ADS-B study is to provide first operational experience of ADS-B in ATCS environment of South Korea and provide practical information to ATCS before deployment of ADS-B in South Korea is considered. Participation in the flight test has been limited to 2 Aircraft of H University which are installed ADS-B equipment and the ground station has installed in Tae-An airport. This test have been experimented according to the pre-arranged flight procedures of Tae-An airport. As a result of the test, it has shown that the number of radio transmitting and the time of radio occupied between controller and pilot are remarkably reduced. Besides, as both pilot and air traffic controller are able to see the traffic information in the vicinity of the aircraft, the test has demonstrated that it is possible for ADS-B not only to decline the controller's workload, but also to enhance pilot situational awareness in the near future.