• Title/Summary/Keyword: 비행 시간

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A Study on loggings of flight time(Focusing on the record of instrument flight) (비행시간 산정에 관한 연구(계기비행 기록을 중심으로))

  • Hwang, Ho-Won;Noh, Yo-Sup
    • The Korean Journal of Air & Space Law and Policy
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    • v.20 no.2
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    • pp.253-276
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    • 2005
  • A pilot logbook is an essential data for proving pilot's flight experience. the reason for maintaining this information is to fulfill the requirement for pilot certificates, manage internationally shared career placement. this study focuses on the instrument flight related items among other flight time items which are included in a pilot logbook. By comparing the way of flight time logging among Korean Aviation Law, Federal Aviation Regulation and Joint Aviation Requirements, this study concludes intensively how to define items for flight time, to amend the definition and to apply the policy in Korea with respect to the pilot logbook.

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A Study on the Flight Test of Airplane Changgong-91 for Korea MOT Type Certification (교통부 형식 증명 획득을 위한 창공-91 비행 시험 수행에 관한 연구)

  • Choi, Byoung-Chul;Lee, Jung-Mo
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.1
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    • pp.81-93
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    • 1993
  • 창공-91의 비행 시험의 목적은 성능 측정과 비행 특성의 확인이며 교통부의 기준은 주로 비행기의 운항에 따르는 안정성에 주안점을 두고 있다. 비행 시험으로 실속 속도와 이착륙 성능 그리고 상승 성능을 측정하여 비행 교범에 수록하였고, 안정성과 조종성의 적절함을 판단하였다. 창공-91 A2기의 비행 시험에 소요된 비행 시간은 81. 5 시간이다. (창공-91 $A_1$기 : 52.8시간)

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Guidance Law to Control Impact-Time-And-Angle Using Time-Varying Gains (시변 이득을 이용한 비행시간 및 충돌각 제어 유도법칙)

  • Lee, Jin-Ik;Jeon, In-Soo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.7
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    • pp.633-639
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    • 2007
  • This paper presents a new homing guidance law based on well-known BPN to achieve an impact time constraint as well as an impact angle constraint. The guidance commands are synthesized by introducing an additional command to control impact-time. The structure of the additional command has a BPN-based loop multiplied by time-varying gains being proportional to the time difference between the required time-to-go and the estimated time-to-go by BPN. Moreover, the proposed homing loop converges to BPN as the time-to-go error is reduced. The performance of the proposed guidance law is evaluated by the computer simulations.

A Study of Paths of the Effects of Adolescents' Part-time Work Experiences on Mild and Serious Delinquency (청소년 아르바이트 경험이 경비행 및 중비행에 영향을 미치게 되는 경로 탐색)

  • Kim, Ye-sung;Kim, Sun-suk
    • Korean Journal of Social Welfare Studies
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    • v.40 no.1
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    • pp.139-161
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    • 2009
  • The purpose of this study was to investigate the paths of the related variables that exert an influence upon the increase in mild and serious delinquencies of part-time work adolescents. Based on differential association theory, social control theory and power resource theory, the research model was composed and analyzed through structural equation model. Data came from survey which was done by fifteen high schools located in Seoul, and 201 questionnaire of returned were used for analysis. The results were congruent with theoretical expectations. The relationship between work hour per week and delinquency was mediated by delinquent propensity of fellow workers, amount of spending money and school adjustment. In conclusion, various theoretical and practical implications for social work practice focusing on the part time work students were discussed. Enforcement of regulation and revision of current law and various ways for helping and supervising working students in school, family and working places are needed.

Effect of Time-to-go Estimate to Impact Time Control Guidance Laws (충돌시간 제어 유도법칙에 대한 잔여비행시간 추정의 영향)

  • Kim, Mingu
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.47 no.8
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    • pp.558-565
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    • 2019
  • A lot of studies on the survivability of missiles have been widely studied, since the technology of modern warships equipped with state-of-the-art defense systems has been improved. The survivability of missiles can be improved by attacking a target simultaneously using multiple missiles. For this reason, impact time control guidance (ITCG) laws have been widely studied. This paper deals with the effect of time-to-go estimate to ITCG laws. In this paper, two kinds of time-to-go estimate are first introduced in two-dimensional and three-dimensional environment and then ITCG laws are derived using the time-to-go estimate. Numerical simulations are performed to analyze the performance of the designed ITCG laws and the effect of time-to-go estimate is discussed.

Homing Guidance Law of Anti-Ship Missiles Using Flight Path Angle (비행 경로각을 이용한 대함 유도탄의 호밍 유도법칙)

  • Jin, Sheng-Hao;Yang, Bin;Hwang, Chung-Won;Park, Seung-Yub;Park, Seung-Je
    • Journal of Advanced Navigation Technology
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    • v.14 no.5
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    • pp.596-603
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    • 2010
  • This paper presents a homing guidance law of anti-ship missiles using flight path angle to achieve an impact time constraint as well as an impact angle constraint. the independent variable in the nonlinear engagement model is change d from the flight time to the heading angle of the missile. The proposed guidance law can home a missile to the target with zero miss distance as well as satisfying both of the impact angle and time constraints. The performance of the proposed guidance law is evaluated by the computer simulations.

The Show up Time in the Development of the Korean Pilots Fatigue Management Program (한국형 운항승무원 피로관리 프로그램의 출두시간에 관한 연구)

  • Lee, Seungyoung;Chung, Seung Sup;Kim, Hyeon Deok
    • Journal of Advanced Navigation Technology
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    • v.25 no.4
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    • pp.280-285
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    • 2021
  • The significance of pilots' fatigue and the attributed risk management had continuously increased over time as the airline industry expanded. Research and legislation efforts associated with pilot fatigue are being taking place actively all over the world. In the developed world such as the United States and European Union etc., the airline pilot fatigue is already being managed by considering the show up time, the number of take offs and landings made, resting period, jet lag etc., when computing flight duty time. In Korea, the flight duty time is only limited by the total number of hours per given period regardless of the flight conditions and environment. Such lack of regulation demand development of a fatigue management program. According to the survey taken from the airline pilots in Korea, it has been found that acquiring foreign policies directly may in turn, increase the risk of fatigue. This research suggest future studies regarding fatigue management program adapted exclusively to Korean domestic flight environment and culture.

A Difference Analysis on Visual Approach Accessibility of Airline Pilots Based on Flight Experience including Non-parametric Statistical Test (정기항공사 소속 조종사의 비행경력에 따른 시계접근능력 차이 분석 : 비모수 통계검정을 포함하여)

  • Lee, Gun-Young;Hwang, Jae-Kap;Jang, Ji-Seung
    • Journal of Advanced Navigation Technology
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    • v.23 no.2
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    • pp.104-113
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    • 2019
  • There are keen competitions among the air operators to recruit competent pilots, which could be adversely affect the safe operation of aircraft. This study is aimed to identify the correlation between the flight experience of the pilot of the air transport operator and competency on visual approach operation. About 2,400 sets of flight training data of several pilots of an air transport operator was analysed for this study. The analysis showed that most captains were able to make stabilized visual approach regardless of his/her flight experience of any type of aircraft, while the first officers were able to make a stabilized visual approach with more than 1,500 hours of flight experience for each rated type of aircraft. This should be considered during making policies for the supply and demand of pilots for the safe operation of air transport.

Performance Analysis of an Electric Powered Small Unmanned Aerial Vehicle (전기동력 소형무인항공기의 성능분석)

  • Lee, Chang-Ho;Kim, Seong-Wook;Kim, Dong-Min
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2010.05a
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    • pp.226-230
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    • 2010
  • In this paper, the performance of an electric powered small Unmanned Aerial Vehicle which has a battery and electric motor is analysed. Aerodynamic data is obtained through flight test and flight performance is predicted. As a result, we present the optimum flight speed for the maximum endurance and predict endurance and range according to the variation of flight speed.

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A Study on the Parameters for Icing Airworthiness Flight Tests of Surion Military Helicopter (수리온 군용헬기의 결빙 감항인증 비행시험을 위한 파라미터 고찰)

  • Hur, Jang-Wook;Kim, Chan-Dong;Jang, Jae-Sang
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.43 no.6
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    • pp.526-532
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    • 2015
  • In order to relieve limitation of flight operation under icing condition and verify its operation in adverse weather condition for Surion, military helicopter developed in Korea, airworthiness certification in icing condition is required. The process of Surion icing certification should be considered by implementation of four methods by step such as CFD analysis, simulated flight tests, artificial icing flight tests, and natural icing flight tests. For Surion icing flight tests, these are required 20~30 sorties and 20~23 hours in artificial icing condition; 20~30 sorties and 20~22 hours in natural icing condition. In addition, to proceed with efficient flight tests, it is necessary to implement artificial icing flight tests in LWC $0.5{\sim}1.0g/m^3;$ natural icing flight tests in less than LWC $0.5g/m^3$.