• 한국정밀공학회지
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• 제33권10호
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• pp.781-787
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• 2016

We introduce FEST (Flight Environment Simulation Test) procedures for precise guided missiles to reliably improve systems. Flight vibration specification was established based on power spectral density curves calculated from flight test data of a high speed precise guided missile. A FEST pre-profile was developed according to flight vibration specification and delivered to a precise guided missile assembly. Vibration responses were measured by installing accelerometers on electronic components vulnerable to dynamic forces. The FEST profile was adjusted by comparing the vibration responses and the flight vibration specification. Subsequently, the FEST profile was repeatedly modified through trial and error, because the responses were similar to the flight environment. The modified FEST profile enabled performance testing of assembled precise guided missiles under simulated flight conditions on the ground, where unexpected errors could be corrected before the flight tests, leading to cost and risk reduction in the development of the precise guided missile system.

• 한국항행학회논문지
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• 제28권4호
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• pp.490-496
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• 2024

비행교육은 항공산업의 발전과 안전을 보장하는 데 필수적인 요소이다. 한국의 항공산업은 급격한 성장을 이루었으며, 이에 따라 전문적인 비행교육의 필요성도 증가하고 있다. 본 논문은 국내 비행교육환경의 현황을 분석하고, 이를 개선하기 위한 방안을 모색하는 데 목적이 있다. 또한, 우리나라 조종사 양성 전문교육기관의 운영방식 및 교육 환경이 학생 교육에 적합하게 구성되었는지 살펴보고 우리나라 조종사 양성 전문교육기관에서 교육을 받는 교육생 및 교관들과 항공종사자를 대상으로 비행교육 인프라에 대한 설문 조사를 통해 국내 비행교육에 대한 인프라 개선에 대한 필요성과 시급성을 조사하여 유의미한 결론을 도출하였다.

• 한국항공우주학회지
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• 제40권6호
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• pp.548-554
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• 2012

항공기 비행조종컴퓨터 탑재 소프트웨어는 항공기의 손실뿐만 아니라 조종사의 생명에도 직결되는 비행안전 필수 소프트웨어로서 정확성과 무결성을 입증하기 위한 검증 및 확인(Verification & Validation)이 요구된다. 특히 비행안전 필수 소프트웨어는 검증을 위해 통합시험 단계에서 실제 환경과 유사한 운용 환경에 노출하여 소프트웨어 내부 상태를 실시간으로 모니터링하기 위한 환경이 요구된다. 본 논문에서는 표준 디버깅 인터페이스인 NEXUS 5001을 이용한 비행안전 필수 소프트웨어의 검증환경 개발에 대하여 기술하였다.

• 한국군사과학기술학회지
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• 제26권3호
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• pp.273-280
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• 2023

Recently electronic safety and arming device(ESAD) has attracted increasing attention due to its design flexibility. However, ESAD can be armed unintentionally due to a malfunction of an external device or interface. Thus ESAD needs an internally generated arming signal independent from the external device. In this paper, a new sensor-hybrid ESAD(SHESAD) with a flight environment sensing function for generating arming signal internally is proposed and a sled test based method is also suggested for evaluating its functions. Through the test results, the operability of the flight environment sensing function was confirmed. Also, it is shown that the proposed test method is suitable for verification of ESAD with the flight environment sensing function.

• 한국항공운항학회지
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• 제31권1호
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• pp.68-78
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• 2023

This study aims to provide information necessary for developing a "Competency-Based Training and Evaluation Plan" for general aviation flight instructors in Korea. General aviation training experts designed a survey by selecting "Behavior Indicators" from the ICAO Flight Instructor Competency Model. This study analyses the importance of Behavioral Indicators, the level of instructor performance, and the training needs for flight instructors. According to the factor analysis, ICAO "Flight Instructor Competency Model" is found as a valid tool to measure general aviation flight instructor competencies. According to the training needs analysis, flight instructors training program needs to be improved on "Training Environment Management", "Teaching Method", and "Interaction" competencies. When compared with trainee group, flight instructors & examiners have a higher training demand for "Teaching & Learning Environment Management". This study suggests the flight instructor training program requires to be reorganized based on the competencies related to the flight instructor duties in the training environments.

• 한국항공우주학회지
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• 제35권9호
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• pp.783-791
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• 2007

FAA AC 120-63 등급 C 또는 FTD 등급 5에 규정된 헬리콥터 모의 비행 훈련장치에 사용될 단일 로터 회전익기의 수학적 모델에 대해 고찰하였다. 선정된 비행 운동 모델의 비행 운동 성능 평가를 통해서 그 유용성을 파악하였다. 이로부터 훈련은 물론 조종 성능시험이 가능한 비행 훈련장치 개발을 통해서 헬리콥터 비행성 평가를 위한 모의 비행 시험환경을 구현하였다.

• 한국항공운항학회지
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• 제21권4호
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• pp.53-61
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• 2013

In-flight service, depending on the perceptions of service satisfaction because ever turns into a variable, which enables service providers the flexibility of a variable in the end flight service to suit your needs to providing comprehensive and proactive services of the crew will be motivated. In addition, the service provider's motivation to work in a confined space on board the flight service characteristics in-flight service will be a major impact on the environment. This service-oriented environment, in-flight service and motivation in order to verify the impact on services in Cape factors as independent variables and the dependent variable service-oriented multi-regression analysis was performed. As a result, the motivation of the crew and the crew of the service-oriented, with a voluntary service crew services dependent variable parameters that affect the behavior of the acts. Services and service-oriented motivation Cape factors significantly influence both the irradiated while the impact on voluntary service and results verification service aesthetics, cleanliness, and physical service environment, only the voluntary services of the crew a positive effect on that the effects were investigated.

• 대한임베디드공학회논문지
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• 제18권6호
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• pp.327-333
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• 2023

Existing studies on the UAV (Unmanned Aerial Vehicle)-based CPS (Cyber Physical System) environment lack forest fire monitoring and forest fire reconnaissance using real-world UAVs. So, it is necessary to monitor forest fires early through CPS based on real-world UAVs with high reliability and resource management efficiency. In this paper presents an MFG (Misstion File Generater) that automatically generates a flight path of an UAV for forest fire monitoring in a CPS environment. MFG generates flight paths based on a hiking trail with a high fire probability due to a true story of an entrant. We have confirmed that the flight path generated by MFG can be applied to the UAV. Also, we have verified that the UAV flies according to the flight path generated by MFG in simulation, with a negligible error rate.

• 한국의류산업학회지
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• 제23권1호
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• pp.118-128
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• 2021

This study used a preliminary survey to help develop an ergonomic flight jacket that is suitable for the working environment and mission performance. The results are as follows. The ergonomic sleeve pattern was designed with a forward 165° incline that considers a shoulder joint direction suitable for the motion; in addition, a closely design opening provided warmth and safety from fire. As a result of the dimensional suitability, pilots evaluated that sleeve length and total length of the developed flight jacket were a little long (p<.01), while flight engineers and crew evaluated that those of the developed flight jacket were appropriate (p<.01). Pilots evaluated that chest circumference and waist circumference were large (p<.05), while flight engineers and crews evaluated that those of the developed flight jacket were appropriate. The evaluation of the motion suitability indicated that pilots, flight engineers and crew found the developed flight jacket more comfortable than the current flight jacket (p<.05, p<.01, p<.001). The evaluation of the usability of pockets and penholders indicated that pilots, flight engineers and crew found the developed jacket easier to use (p<.01). The flight engineers and crew evaluated that the appearance of the developed flight jacket was better than the current flight jacket (p<.05). The results of this study show that the difference of environment and mission performance has a significant influence on evaluation; therefore, it is necessary to develop separate military uniforms that included a winter flight jacket to reflect the needs of each group.

• 한국항공우주학회지
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• 제37권7호
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• pp.701-708
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• 2009

개발된 비행제어컴퓨터(DFLCC: Developed Flight Control Computer)의 비행제어법칙은 고등훈련기급 항공기의 시제 최종 형상의 비행제어소프트웨어(OFP: Operation Flight Program)를 기반으로 개발되었다. 비행제어법칙은 상용 개발 툴을 이용하여 GUI(Graphic User Interface) 환경에서 설계되며, C 코드로 변환되어 OFP 에 반영된다. 그리고 OFP는 정형화된 검증절차를 통하여 검증되는데, 검증과정을 거치기 전에 비실시간 환경에서 C코드로 변환된 비행제어법칙과 기반이 되는 비행제어법칙의 상사성(similarity)을 검증하고, 구성된 HILS(Hardware In-the-Loop Simulator) 환경의 신뢰성(reliability)을 사전에 검증하는 절차가 필요하다. 비행제어법칙의 상사성은 비실시간 환경에서 고등훈련기급 항공기의 시제 최종 버전의 비행제어법칙과 개발된 비행제어법칙의 응답특성을 상호 비교하여 검증된다. 또한, 구성된 HILS 환경의 신뢰성은 비실시간 시뮬레이션 툴을 기반으로 HILS 결과와 항공기 응답특성을 비교하여 검증된다. 본 논문에서는 항공기 응답을 직접 비교함으로써 개발된 비행제어법칙의 상사성과 HILS 환경의 신뢰성을 검증하였다.