• 한국항공운항학회:학술대회논문집
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• 2004.11a
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• pp.161-166
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• 2004

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.35 no.10
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• pp.948-956
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• 2007

It is important during FSD(Full Scale Development) period to verify whether the aircraft system function meets the aircraft requirements and functional performance. Especially, the functionality of the integrated propulsion system should be verified to evaluate the compatibility with aircraft. Various flight tests such as the engine airstart test, the engine horsepower extraction test, the backup throttle functionality test had been performed to evaluate the engine/aircraft compatibility with T-50 during FSD period. Through such flight tests, it was confirmed that the propulsion system of T-50 was properly designed and installed to the aircraft. This paper shows description on each flight test item, test procedure and test results. It is expected that this paper could be a reference for preparing the propulsion flight test in other aircraft developments.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.42 no.9
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• pp.773-778
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• 2014

Aircraft communication system which provides internal communications between pilots in an aircraft and external communications between pilots and operators in ground tower with them. It is very important equipment in terms of mission and safety. It wouldn't meet performance requirements with only functions of transmission and receiving of signals. It should provide highly clear voice quality without any noise. This paper analyzes the cause of noise during internal communications and summarizes the design changes applying single point ground concept to solve the problem. It also describes the results of fight test to verify the design changes.

• Review of KIISC
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• v.28 no.6
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• pp.39-44
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• 2018

우리나라 방위산업은 고등훈련기, 잠수함 등을 수출할 정도로 발전했으며, 방산 기술력은 선진국 대비 80% 수준으로 평가받고 있다. 이렇게 방위산업이 발전함에 따라 국가 안보상 중요한 정보를 유출하려는 시도도 증가하고 있다. 이러한 상황에서 정부는 방산업체에서 보유한 중요 정보를 보호하기 위한 정책들을 시행하고 있으나 방산업체별 다양한 특성을 고려하지 않은 채 획일화된 정책을 추진함으로써 투자 대비 효과성이 떨어지는 것이 현실이다. 따라서, 본 논문에서는 보안에 대한 투자 대비 효과성을 높이기 위해 방산업체 특성을 고려한 차등화 된 보안정책 개발에 활용할 수 있도록 핵심 평가 요소를 도출하고 요소별 가중치를 산출하는데 목적이 있다.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.12 no.3
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• pp.1171-1177
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• 2011

The purpose of this study was to verify the effect of neurofeedback training on adolescence groups that are different in sex. The experiment was carried out with 45 students who living in Yong-in of Kyonggi Province. From November 2009 to March 2010, each were under training about 20-25 times, 2-3 times a week, during 20 to 50 minutes, was conducted by limiting training. Statistical data collected were processed with the SPSS 12.0. For the purposes of t-test showed that differences in the effects of sex. The result, The effects of neurofeedback training, according to the sex differences were confirmed. only boys showed stress resistance quotient, only girls showed emotional quotient. they also have differences in some part of cerebral cortex that are responsible for stress and emotion. As a result, neurofeedback training affects the prefrontal lobe.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.11
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• pp.70-75
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• 2006

The cabin pressurization system response should be consistent with the design limits such as the cabin pressure schedule, the pressure regulation tolerance, the maximum rate of pressure change during normal and abnormal operation and the maximum cabin air inflow rate change. In this paper, the results of pressure loss analysis and flight test for cabin pressurization system of T-50 advanced trainer are introduced. The pressure tolerance at unpressurized condition using calculated exit area of pressurization components through pressure loss analysis is predicted. Pressurization components of D company are selected and the predicted pressure tolerance is in good agreement with flight test results. Finally, T-50 pressurization system is verified by some flight tests of T-50 advanced trainer to comply with various pressurization design criteria of MIL-E-18927.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.36 no.11
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• pp.1104-1111
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• 2008

The supersonic advanced trainer based on digital flight-by-wire flight control system uses aircraft flight information such as altitude, calibrated airspeed and angle of attack to calculate flight control law, and this information is measured by IMFP(Integrated Multi-Function Probe) equipment. The information has triplex structure using three IMFP sensors. Final value of informations is selected by mid-value selection logic to have more flight data reliability. As the result of supersonic flight test, pitch oscillation is occurred due to IMFP noise when altitude hold autopilot mode is engaged. This tendency may affect stability and handling quality of an aircraft during autopilot mode. This paper addresses autopilot control law design to remove pitch oscillation and these control laws are verified by non-real time simulation and flight test. Also, pitch response characteristics of pitch attitude hold autopilot mode is improved by upgrading the control law structure and feedback gain tuning during bank turn.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.14 no.12
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• pp.6309-6316
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• 2013

Morbidity, mortality, mental health and problem behavior appears to be high in adolescence, but there is no proper intervention. This quasi-experimental study examined the effects of the neurofeedback training on the general health status, mental health and problem behavior, and the brain function quotient through structured questionnaires and brain waves of 11 high school students (experimental group 5, control group 6). The study was conducted at I high school in Seoul from September to December, 2012. The subjects participated in the neurofeedback training twice a week for a total of 20 sessions by trained researcher. The data was analyzed using paired t-test or Wilcoxon signed rank test depending on the normality using SPSS 20.0. Significant improvement was observed in the emotion quotient and stress resistance quotient (left, right) among the brain function quotient, but not in the general health status, mental health and problem behavior.

• Defense and Technology
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• no.5 s.291
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• pp.22-29
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• 2003

현재 방산업체 위주의 방산물자 수출 수주활동은 한계에 직면하고 있으며 우리가 향후 수출하려는 장갑차, 전차, 초등/고등 훈련기, 신형 자주포, 함정 등과 같은 고가의 시스템 장비는 방산업체의 노력만으로는 수주성공이 어려워 정부의 적극적인 지원이 요구된다고 할 수 있다. 그 동안 우리 정부에서도 방산물자 수출의 중요성과 정부의 역할을 인식하고 상당한 노력을 기울여 왔음에도 불구하고 아직까지도 정부차원의 방산물자 수출전담 지원기구가 없으며, 방산물자 수출을 위한 금융지원제도의 미약, 국제 방산 협력의 미흡, 독자적인 수출전략 품목의 부족, 그리고 해외시장에 대한 정보획득 제한 등의 문제점으로 인해 정부.군.업체가 공동으로 수출 마케팅을 수행하기 어려운 상황이다.

• Proceedings of the KSME Conference
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• 2003.11a
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• pp.1384-1387
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• 2003

Pressurization test is usually required in aircraft full-scale static test. There are several test conditions including pressurization of cockpit, fuselage fuel tank, air inlet duct for T-50 full-scale static test. In this paper, the test conditions, equipment, piping analysis for the pressurization test are introduced. Tank simulation test is performed to verify the validity of piping analysis and to find good tuning parameters for the pressurization channel in the servo controller. Several test setup for pressurization of T-50 test is introduced. Test article volume is filled by form, $60%{\sim}80%$ volume is reduced for the T-50 full-scale static test. Pressurization system is connected to servo controller which also controls hydraulic actuator. Load and pressure control is synchronized by using the same servo controller during T-50 test. Typical control result for pressurization test condition is shown. Pressurization tests of T-50 full-scale static test was completed successfully.