• 유통과학연구
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• 제18권3호
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• pp.43-51
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• 2020

Purpose: This study demonstrated and analyzed the role of distributive justice and procedural justice in explaining the organizational effectiveness of flight attendant. In addition, analyzing the role of the airline type in the coordination between reward justice and organizational effectiveness. Research design, data and methodology: An abstract is the impact relationship between the reward justice and organizational effectiveness of flight attendant and the adjustment effect of the airline type was reviewed. To examine these research models, samples were collected from 281flight attendants during Nov, 2019. Results: Reward justice has a positive effect on organizational effectiveness, and the types of airlines have a meaningful adjustment effect in terms of the effect of reward justice on organizational effectiveness. Conclusions: Procedural justice and distributive justice have positive influence on two sub factors of organizational effectiveness of the flight attendant. It suggests that the standards, procedures and processes of compensation must be fair, the degree of effort, the stress or the tension of the flight attendant should be considering, and it is necessary for the airline to respect the personality of the flight attendant and provide them with accurate compensation information in a timely manner. This will increase the awareness of reward.

• 한국군사과학기술학회지
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• 제22권4호
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• pp.536-544
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• 2019

During the assembly and function inspection of missile system, flight simulation process is required. In the conventional flight simulation check of missiles, an inertial navigation system simulator was used to transmit the navigation output data acquired in HILS. There are several disadvantages in terms of check configuration complexity and data synchronization when using the simulator. So we proposed a new flight simulation method that utilizes the nonvolatile built-in memory of the aviation control unit. The data processing procedure and operation procedure of the proposed method for type I and type II missiles are presented. And we analyzed the causes of the difference between proposed method result and the HILS result for type II missile. By comparing the results obtained by the experiments using the proposed method with the results of HILS, the validity of proposed method was confirmed.

• 한국항공운항학회지
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• 제32권1호
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• pp.103-108
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• 2024

Despite the development of the aviation industry, aircraft accidents caused by human errors by flight crews continue to occur. In order to reduce such human error accidents, it is important to strengthen flight-related regulations and establish a safety culture in which pilots themselves seek to ensure flight safety, rather than requiring flight crew members to follow them. In this study, the sub-concept of safety culture was classified into three latent variables (safety management, safety atmosphere, and process culture) and eight measured variables to investigate the safety culture awareness of domestic flight crew. The survey results were analyzed by type of airline and flight crew. The purpose of this study is to present a plan to improve the performance of revitalizing the safety culture of domestic flight crew through an empirical comparative analysis according to the number of flight hours and years of service at the airline.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2005년도 제24회 춘계학술대회논문집
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• pp.219-224
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• 2005

본 연구는 CRW형식 무인항공기 추진시스템의 밸브 작동을 고려한 비행모드에 따른 천이성능특성을 파악하기 위해 SIMULINK를 이용하여 모델링 하였다. 주 엔진시스템의 천이모사에는 ICV 방법이 적용되였다. 그리고 밸브 시스템은 로터리 덕트와 메인 덕트로 빠져나가는 유량을 제어하는 시스템으로서 밸브를 통해 로터리 덕트로 빠져나가는 유량과 메인 덕트를 빠져나가는 유량이 합은 터빈의 출구 유량과 같다는 가정하에 수행 되었으며, 이때 밸브각 변화에 따른 손실, 유량 및 유효 면적 등이 고려되었다. 성능해석은 비행 천이 영역인 고도 1Km 비행 마하수 0.1에서 엔진최대회전수시 회전익 모드에서 고정익 모드로 변환시외 고정익 모드에서 회전익 모드로 변환 경우들이 수행되였다.

• 한국추진공학회지
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• 제9권3호
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• pp.127-132
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• 2005

본 연구는 CRW형식 무인항공기 추진시스템의 밸브 작동을 고려한 비행모드에 따른 천이 성능 특성을 파악하기 위해 SIMULINK를 이용하여 모델링 하였다 그리고 밸브 시스템은 로터리 덕트와 메인덕트로 빠져나가는 유량을 제어하는 시스템으로서 밸브를 통해 로터리 덕트로 빠져나가는 유량과 메인덕트를 빠져나가는 유량의 합은 터빈의 출구 유량과 같다는 가정 하에 수행되었으며, 이때 밸브 각 변화에 따른 손실, 유량 및 유효 면적 등이 고려되었다. 성능 해석은 비행 천이 영역인 고도 1km 비행 마하수 0.1에서 엔진 최대회전수시 회전익 모드에서 고정익 모드로 변환되는 경우와 고정익모드에서 회전익 모드로의 변환되는 경우들이 수행되었다.

• 한국항공운항학회지
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• 제30권4호
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• pp.92-97
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• 2022

In the Aviation Safety Act, the part about fatigue management of Flight dispatcher was added as an amended law. Prior to the amendment of the Act, the regulations on fatigue of flight dispatcher governed by the FOM approved and reported by airlines according to the Ministry of Land, Infrastructure and Transport, but were enforced by law from June 9, 2021. In this study, the scope and work type of flight dispatchers are checked, and unlike flight attendants, it is intended to consider legal working hour management measures for flight dispatchers according to the enforcement of the fatigue management act.

• 유통과학연구
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• 제15권8호
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• pp.37-46
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• 2017

Purpose - Many studies have shown the effects of the external images of female flight attendants on the customers' satisfaction. Recently, the perception of male flight attendants has become more important and positive, and airlines are hiring a significant number of male flight attendants every year. Due to the lack of research on the male flight attendant, however, the images of male flight attendants were investigated for this study. Research, design, data and methodology - Using survey techniques with 204 respondents, this study used analytical data based their resulting analysis. Results - The study examined whether the image of the male flight attendant affects the cognitive and emotional perceptions of customers. The focus of the present study is the external image of the male flight attendant, and the following image-component divisions were formed: hairstyle, body type, uniform, speech, and facial expression. Conclusions - The study purpose sought to determine whether the image of the male flight attendant exert effects on the emotional and cognitive images of airlines, and if these images have a positive effect on the customers' satisfaction and loyalty for an airline, so that airlines can use the external image of the male flight attendant to help with its own image reinforcement.

• 한국경영과학회지
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• 제39권2호
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• pp.37-48
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• 2014

Fighter squadron flight scheduling is the integrated air operation plan that is an important role for improving pilot's flight skill and maintaining combat readiness by efficient using available all air resources including pilot, aircrafts, air-weapons, fuel and supporting facilities etc. Korea airforce, however, has a limit as to an effective flight operation due to manual flight scheduling with scheduler's own experience and intuition. Therefore, in our study, we propose the optimization model of flight scheduling based on mixed integer programming. This model includes several constraints of realistic and essential quantified data related with flight schedule and can assign appropriate pilots optimally which are distinctive three type's solutions : flight, alert and duty crew schedules. Proposed solution method can be improved pilot's capability and allocated further air resources systematically and efficiently. In addition, it can be reduced a workload of flight scheduler and minimized obstructed factors of flight safety. Finally, we demonstrate the experiment's results for the check of efficiency and validity of this model.

• 한국항공우주학회지
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• 제33권4호
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• pp.91-99
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• 2005

ALQ-X ECM 포드를 KF-16D와 RF-4C 항공기에 장착하기 위한 비행적합성 인증을 수행하였다. MIL-HDBK-1763에 부합하는 외부장착 스토어 인증 절차를 계획한 후 유사성 분석, 기존 스토어 질량 및 관성모멘트 분석, 구조해석 및 시험, 지상진동시험 및 플러터해석을 수행하여 비행시험 수행에 대한 안전성을 확인하였다. ALQ-X 장착 형상을 대표하는 비행 형상으로 MIL-HDBK-1763 Test 250 비행시험을 하였다. ALQ-X 장착 전, 후의 비행특성 차이를 분석하여 조종성을 평가 하고 구조건전성과 내구성은 계측데이터를 함께 분석하여 ALQ-X가 KF-16D 및 RF-4C와 적합성이 있음을 확인하였다. 그 결과로서 ALQ-X를 기존에 인증된 ALQ-88 및 ALQ-119와 동일하게 운용할 수 있음을 인증하였다. ALQ-X 비행인증 결과로서 도입 전투기에 대한 TYPE III 비행적합성 인증, 시험데이터를 사용한 플러터 해석 프로그램을 개발, MIL-STD-1553B 데이터버스를 사용한 비행시험 데이터를 획득할 수 있는 기법과 같은 기술적 성과를 거두었다. 본 비행인증 결과는 향후 국내에서 수행할 Type III 형식의 외부장착 스토어 비행인증의 모델케이스가 될 것으로 기대한다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2007년도 춘계학술대회A
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• pp.891-896
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• 2007

This paper contained the flight test calibration for the airspeed indicator and the altimeter of the light airplane ChangGong-91, which is the first type certified aircraft from Korean Ministry of Construction and Transportation, as a part of the flight test validation. The flight test for airspeed position error calibration was performed using tower fly by method in order to calibrate swivel head testboom which is attached to the right wing tip of the airplane, and using system to system method for airspeed indicator. The altimeter calibration was calculated using flight test data for airspeed calibration. The flight test was conducted at the basis of the 'Korean Airworthiness Standard' regulation of Korean Ministry of Construction and Transportation.