• Title/Summary/Keyword: Emergency Aircraft

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A Study on the Design and Validation of Pilot Activated Recovery System to Recovery of an Aircraft Unusual Attitude (항공기 자세회복을 위한 자동회복장치 설계 및 검증에 관한 연구)

  • Kim, Chong-Sup;Cho, In-Je;Kang, Im-Ju;Hur, Gi-Bong;Lee, Eun-Yong
    • Journal of Institute of Control, Robotics and Systems
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    • v.14 no.3
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    • pp.307-317
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    • 2008
  • Relaxed static stability(RSS) concept has been applied to improve aerodynamic performance of modem version supersonic jet fighter aircraft. Therefore, flight control system are necessary to stabilize an unstable aircraft and provides adequate handling qualities. Also, flight control systems of modem version aircraft employ a safety system to support emergency situations such as a pilot unknown attitude flight conditions of an aircraft in night flight-testing. This situation is dangerous because the aircraft can lose if the pilot not take recognizance of situation. Therefore, automatic recovery system is necessary. The system called the "Pilot Activated Recovery System" or PARS, provided a pilot initiated automatic maneuver capable of an aircraft recoveries in situations of unusual attitudes. This paper addresses the concept of PARS and designed using nonlinear control law design process based on model of supersonic jet trainer. And, this control law is verified by nonlinear analysis and real-time pilot evaluation using in-house software. The result of evaluation reveals that the PARS support recovery of an aircraft unusual attitude and improve a safety of an aircraft.

A Study on Design and Validation of Pilot Activated Recovery System to Recover Aircraft Abnormal Attitude, Altitude and Speed (항공기 비정상 자세, 고도 및 속도 회복을 위한 자동회복장치 설계 및 검증에 관한 연구)

  • Kim, Chong-Sup;Kang, Im-Ju
    • Journal of Institute of Control, Robotics and Systems
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    • v.14 no.12
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    • pp.1302-1312
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    • 2008
  • Relaxed Static Stability(RSS) has been applied to improve flight performance of modern version supersonic jet fighters. Flight control systems are necessary to stabilize an unstable aircraft and to provide adequate handling qualities. Also, flight control systems of modern aircraft employ many safety measure to cope with emergency situations such as a pilot unknown attitude flight conditions of an aircraft in night flight-testing. This situation is dangerous because the aircraft can lose if the pilot not take recognizance of situation. The system called the "Pilot Activated Recovery System" or PARS, provided a pilot initiated automatic maneuver capable of an aircraft recoveries in situations of unusual attitudes, speed and altitude. This paper addresses the concept of PARS with AARS(Automatic Attitude Recovery System), ATCS(Automatic Thrust Control System) and MARES(Minimum Altitude Recovery Estimation System), and this control law is designed by nonlinear control law design process based on model of supersonic jet trainer. And, this control law is verified by real-time pilot evaluation using an HQS(Handling Quality Simulator). The result of evaluation reveals that the these systems support recovery of an aircraft unusual attitude and speed, and improve a safety of an aircraft.

Analysis and Improvement of False Alarm Phenomenon of Emergency Hydraulic Warning Light by Shielded RF Radiation Signal (RF 방사 신호 차폐를 통한 비상 유압경고등의 비정상 점등 현상의 원인분석 및 개선)

  • Jung-Hyuk Kwon;Gyeong-Nam Kim;Byeong-Kwon Jeon;Wang-Sang Lee
    • Journal of Aerospace System Engineering
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    • v.17 no.1
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    • pp.68-78
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    • 2023
  • In this paper, improvement measures were studied for false alarm (abnormal lighting) of emergency hydraulic warning light due to RF radiation signals in aircraft. When the warning lamp of the emergency hydraulic system is lit during flight due to electromagnetic interference caused by RF radiation signals, it affects flight mission and safety which can result in efficiency degradation and maintenance of flight mission. For false alarm of emergency hydraulic warning light, root cause analysis and troubleshooting were carried out. By shielding a composite strip under fuselage of the aircraft located in the path of the RF radiation signal, the RF radiation signal flowing into the emergency hydraulic indicator was blocked. Results of applying the improvement method through ground and flight monitoring were also described.

The study of the possibility Emergency Landing for LSA in Marado (마라도에서의 경량항공기 비상착륙 가능성에 대한 연구)

  • Shin, Dai-Won;Lee, Gi-Moung
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.24 no.3
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    • pp.19-25
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    • 2016
  • In this study, we surveyed the Marado status of the availability of emergency runway for the LSA, through site visits. For the future progress Marado flight tour operation, for LSA of 4 models with respect to just in case there was an emergency situation analysis of the availability of emergency runway. We analyzed the problems of the sloping runway with the changing elements for the kinetic and potential energy. The Bingo and CH-650 models of LSA are usability emergency runway of Marado for take-off and landing. But the AT-4 and CTLS models of LSA are limited or impossible to use emergency runway of the Marado.

Development of Weapon Control Unit using a Design Technique for Sequence Control Circuits (순차 제어회로 설계기법을 이용한 무장제어장치 개발)

  • Park, Deok-Bae;Kim, Hyung-Shin
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.9 no.3
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    • pp.632-637
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    • 2008
  • On board Weapon Control Unit for a military aircraft, as a core equipment of the Weapon Management System, generates signals for selective jettison, emergency jettison and rocket fire and controls the external stores according to a pilot's weapon selection, aircraft's flight status and external store's installation status. This paper describes about detail design process and performance evaluation for Weapon Control Unit developed by a sequence control circuit design methodology.

A Security-Enhanced Storing Method for the Voice Data in the Aircraft (항공기에서 보안 강화된 음성 데이터 저장 방식)

  • Cho, Seung Hoon;Suh, Jeong Bae;Moon, Yong Ho
    • IEMEK Journal of Embedded Systems and Applications
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    • v.6 no.4
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    • pp.255-261
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    • 2011
  • In this paper, we propose a security-enhanced storing method for the voice data obtained during the flight. When an emergency occurs during flight, the flight data in the storage device such as DTS or Blackbox can be exposed to antagonist or enemy. Currently, zeroize function is embedded in these devices in order to prevent this situation. However, this could not be operated if the system is malfunctioned or the pilot is wounded in the emergency. In order to solve this problem, the voice data compressed by the ADPCM is encrypted in the proposed method composed of the AES algorithm and a reordering method. The simulation results show that the security for the voice date is further enhanced due to the proposed method.

A Scheme of Crisis Management for National Aviation Safety (국가차원의 항공안전위기관리 방안)

  • Kim, Yeon-Myung;Hong, Seok-Jin;An, Hyuck-Soo
    • Journal of Korean Society of Transportation
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    • v.23 no.5 s.83
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    • pp.27-34
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    • 2005
  • To develop a crisis management for aviation safety, this study has defined crisis management includes risk management which is eliminates or lowers risks prior to accidents and emergency response after the accidents. A risk management model was developed through wide surveys for aviation hazards including aircraft operation, ATC, and airport operation, etc. The crisis management could not be effective by only using a pre-active risk management. It should also conduct using a pro-active response system. In addition, this study also suggested schemes of development for national emergency response through case studies of aircraft accidents.

Suggestions for the Improvement of Aviation and Railway Accident Investigation Board in Korean (항공사고조사위원회의 업무개선에 대한 제언)

  • Han, KyoungKeun;Choi, YounChul
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.25 no.4
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    • pp.187-194
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    • 2017
  • ICAO Universal Safety Oversight Audit Programme is a comprehensive evaluation for aviation safety matters, including aircraft operation, licensing and aircraft incident/accident investigation. As this programme is measures aviation safety level of States, there is a need to meet international standards, especially in the field of aircraft incident/accident investigation. This research discusses points required to satisfy international standards, which are independence and autonomy of an accident investigation board, the lack of the enough number of investigators and efficient management of those personnel, the effective composition and use of an investigation report, an accident investigation itself to build big data and the creation of a cooperation system among States. This paper suggests various opinions in order to enhance aviation safety especially through aircraft accident investigations, using case studies from the US, UK and Japan.

In-Flight Cardiopulmonary Resuscitation and COVID-19 (기내 심폐소생술과 COVID-19)

  • Kim, Jung Eon
    • Korean journal of aerospace and environmental medicine
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    • v.31 no.3
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    • pp.68-72
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    • 2021
  • As the number of passengers using aircraft increases around the world, there may be more medical measures needed within the aircraft. These medical measures may also include measures against serious situations such as cardiopulmonary resuscitation (CPR). However, since the environment is different from the hospital in the aircraft, it may be difficult to cope with such a situation. Moreover, such in-flight CPR may become more difficult at a time when the proportion of out-ofhospital CPR is decreasing due to the recent COVID-19 pandemic. In this paper, I would like to summarize how in-flight CPR is performed and review the main discussions on CPR in the COVID-19 pandemic, and finally suggest how to perform a safe CPR in the COVID-19 situation.