• Title/Summary/Keyword: Helicopter pilots

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The Effect on Safety Perception with Ultra Light UAV Pilot's Educational Environment Satisfaction : Including the DREEM Model (초경량 무인비행장치 조종자의 교육환경 만족도가 안전의식에 미치는 영향 : DREEM 모형을 포함하여)

  • Jung, Hyung-hoon;Kim, Kee-woong;Choi, Youn-chul
    • Journal of Advanced Navigation Technology
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    • v.23 no.2
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    • pp.114-124
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    • 2019
  • The drone market, an unmanned aerial vehicle, is rapidly expanding and developing into an important area related to the huge changes in the traffic system of the future. With various technologies on the fourth industrial revolution, including drones, mentioned at the Davos Forum in January 2016, interest in drones is emerging as an explosive demand for national certificates. The number of drone pilots, which was only 400 in 2015, is continuing to surpass 17,000 as of 2018. Therefore, this study analyzed the safety perception of the pilots based on the DREEM (Dundee ready environmental assessment) model designed to evaluate the educational environment along with the current state of drone education in Korea. This led to the conclusion that the high level of satisfaction of the pilot with the educational environment contributes to the overall safety perception, including compliance with procedures.

Effects of Meteorological Conditions and Self-instruction on Anxiety and Performance of Helicopter Pilots in Flight (기상 조건과 자기 교시가 조종 중인 헬리콥터 조종사의 불안 및 수행에 미치는 영향)

  • MunSeong Kim;ShinWoo Kim;Hyung-Chul O. Li
    • Science of Emotion and Sensibility
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    • v.26 no.4
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    • pp.29-40
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    • 2023
  • Anxiety is known to upset the balance of the attentional system and prioritize the stimulus-driven system over the goal-directed system; however, self-instruction induces goal-directed behavior with the self-regulation effect. This study verified the effects of meteorological and self-instruction conditions on pilot anxiety and flight task performance for in-service pilots in a virtual reality environment. The meteorological conditions were divided into visual meteorological and very low visibility conditions, and the flight tasks were conducted by varying whether or not self-instruction was performed. The experiment results reveal that anxiety and heart rate were higher, and the performance of the flight task was lower in the very low visibility condition. However, anxiety and heart rate were lower, and the performance of the flight task was higher in the self-instruction condition. This result suggests that accidents due to difficulty in flight may increase because of anxiety, but such accidents may decrease because of flight performance improvement by self-instruction.

Study on Importance of Safety Management Factors in Aircraft Using Business (항공기 사용사업에서의 안전관리요소의 중요도에 관한 연구)

  • Byeon, A-Reum;Cho, Young-Jin;Choi, Youn-Chul
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.24 no.2
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    • pp.68-73
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    • 2016
  • 2016, in total 53 corporations operate 160 aircraft. Since 2000, 52 accidents occurred in these corporations. This number takes 20.2% out of in total 257 accidents. Especially in 2016, in two(2) accidents, two(2) aircraft and people onboard were damaged. According to accident reports of aircraft using service, in most cases actions against common sense were connected to accidents. This means that attentions of managers or pilot would have protected accidents. On the basis of such background, this research analyses accidents cases of corporations operating aircraft by utilizing ahp. According to this anlysis, unlike scheduled and unscheduled airlines, pilots in command (0.109) and assisting crew (0.105) in Liveware have taken the most importance. Operational procedure (0.100) in Software and a controlling system (0.086) in Hardware have shown the second most importance. This result demonstrates that in case of corporations operating aircraft require safety management at different level than airlines.

Design of Aircraft Internal On-glass Antennas (항공기용 내장형 온-글래스 안테나 설계)

  • Kang, Woo-Joon;Choo, Ho-Sung;KIim, Young-Gi;Kang, Ho-Won
    • Journal of the Institute of Electronics Engineers of Korea TC
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    • v.46 no.12
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    • pp.65-71
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    • 2009
  • In this paper, we propose an aircraft on-glass antenna for FM radio reception. To obtain broad matching bandwidth, we employed a multiple loop as the basic antenna structure, and the shape of the loops mimics the frame of a window in order to ensure pilots' field of view as large as possible. The detailed design parameters of the multi-loop structure were determined using a Pareto genetic algorithm with a full wave EM simulation tool. The optimized on-glass antenna was built and installed on a Korean utility helicopter (KUH) The measurement results showed a half power matching bandwidth of about 63.3 %, average vertical bore-sight gain of about -12.98 dBi in the FM band.

A Study on Winter Season Usability Performance Improvement of Flapper Valve for KUH-1 (한국형 기동헬기 동계운용능력 향상을 위한 플래퍼밸브 개선연구)

  • Choi, Jae Hyung;Chang, In ki;Shim, Dai Sung;Ahn, Jeong Min
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.44 no.1
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    • pp.49-56
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    • 2016
  • Flapper Valve of Korean Utility Helicopter(KUH-1) is an essential equipment in Environmental Control System(ECS) for pilot to perform flight mission. It provides pilots and crews with heating, ventilating and air conditioning. It has function of maintaining room temperature to sustain operational capability for pilot and crew. This paper summarizes pilot comments in flight test which are classified by cause of occurrence and the troubleshooting process about each comment. It also describes design improvements which was derived from troubleshooting and suggests verification results of flight test at low temperature.

The Localization Development for Korean Utility Helicopter's On-Board Inert Gas Generation System (한국형 기동헬기 불활성가스발생장치 국산화 개발)

  • Ahn, Jong-Moo;Lee, Hee-Rang;Kang, Tae-Woo;Choi, Jae-Ho
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.18 no.7
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    • pp.662-669
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    • 2017
  • Military rotary aircraft are heavily exposed to projectile environments due to their mission characteristics, and fires caused by fuel leaks after shooting are linked directly to the loss of human life. To improve the survivability of pilots and crews, the fuel tank in rotary aircraft must have gunfire resistance and anti-explosion characteristics. Gunfire resistance can be satisfied by applying a self-sealing cell to a fuel tank. Anti-explosion can be satisfied by reducing the oxygen concentration in an explosive area and suppressing the generation of combustible fuel vapor by minimizing the evaporation rate of the fuel by heat. A Korean utility helicopter applies anon-board inert gas generation system to meet the anti-explosion requirements for ballistic impact. The generator fills the fuel tank with an inert gas and reduces the oxygen concentration. This paper describes the overall development process of the OBIGGS developed in accordance with the localization process of weapon components. OBIGGS was developed/manufactured through domestic technology, and the performance was found to be equal to or better than that of the existing products through single performance tests and aircraft mounting tests.

A Study on Improvement about abnormal display of Multi Function Display for KUH (한국형 기동헬기 다기능시현기의 이상시현 개선에 관한 연구)

  • Kim, Young Mok;Chang, Joong Jin;Jun, Byung Kyu;Kim, Chang Young;Kim, Tae Hyun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.42 no.4
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    • pp.344-350
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    • 2014
  • Multi Function Display(MFD) of Korean Utility Helicopter(KUH) is the component of mission management/display control system and displays image information(navigation, flight, survivability, digital map, maintenance) acquired from Mission Computer(MC) while the aircraft is operated. It is an essential equipment for pilots to perform flight mission and it has functions of display scene control, data display, built in test(BIT) and brightness control. In this paper, it is analyzed the cause of abnormal display(flickering) on MFD and summarized the design changes to solve the defect. It is also described system safety analysis and suggested verification results of flight/ground test.

A Study on Voice Communication Quality Improvement of Intercom System for KUH (한국형 기동헬기 내부통화장치의 통화품질 향상에 관한 연구)

  • Kim, Young Mok;Chang, Joong Jin;Jun, Byung Kyu;Kim, Chang Young;Jeong, Jin Woong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.41 no.12
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    • pp.1002-1010
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    • 2013
  • Intercom System(ICS) of Korean Utility Helicopter(KUH) is an essential equipment for pilot to perform flight mission and it consists of communication system of KUH with VHF-FM radio set and U/VHF-AM radio set. It provides pilots and crews with internal communication, external communication and audible alarm. It has function of controlling volume and selecting two communication modes, normal mode and backup mode. This paper summarizes pilot comments in flight test which are classified by cause of occurrence and the troubleshooting process about each comment. It also describes design improvements which was derived from troubleshooting and suggests verification results of flight test.