• Title/Summary/Keyword: fighter

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Multi-functional Fighter Radar Scheduling Method for Interleaved Mode Operation of Airborne and Ground Target (전투기탑재 다기능 레이다의 공대공 및 공대지 동시 운용 모드를 위한 스케줄링 기법)

  • Kim, Do-Un;Lee, Woo-Cheol;Choi, Han-Lim;Park, Joontae;Park, Junehyune;Seo, JeongJik
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.49 no.7
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    • pp.581-588
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    • 2021
  • This paper deals with a beam scheduling method in fighter interleaving mode. Not only the priority of tasks but also operational requirements that air-to-ground and air-to-air search tasks should be executed alternatively are established to maximize high-quality of situational awareness. We propose a real-time heuristic beam scheduling method that is advanced from WMDD to satisfies the requirements. The proposed scheduling method is implemented in a simulation environment resembling the task processing mechanism and measurement model of a radar. Performance improvement in terms of task delay time is observed.

Convergence and Integration Review of Fire fighter Image through Disaster Movies (재난 영화를 통해 본 소방관 이미지에 대한 융·복합적 고찰)

  • Lee, In-Seob;Kim, Jee-Hee;Kim, Yun-Jeong
    • Journal of the Korea Convergence Society
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    • v.8 no.2
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    • pp.91-97
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    • 2017
  • The purpose of the study was to investigate the fire fighter image through disaster movies in Korea and other countries. From September 1 to 7, 2016, the movie search methods were carried out using movie title and key words via Wikipedia and various internet web sites from 1903 to 2016. The results included that the fire fighters had been considered as the precious person of volunteer activity regarding fire suppression, investigators, and self-sacrifice. Through the convergence and integration review of the disaster movie, this research suggested that the national based establishment of the welfare and safety system for the posttraumatic stress disorder(PTSD) and critical incident stress management(CISM) education program. This study will provide the basic data for the development of welfare and safety management for the fire fighters and let the people know the sacrifice of the fire fighters including the motto, "First in and the last out".

Study on the Health Status of the Residents near Military Airbases in Pyeongtaek City (평택시 군용비행장 주변지역 주민건강조사)

  • Kim, Hyun-Joo;Roh, Sang-Chul;Kwon, Ho-Jang;Paik, Ki-Chung;Rhee, Moo-Yong;Jeong, Jae-Yun;Lim, Myung-Ho;Koo, Mi-Jin;Kim, Chang-Hoon;Kim, Hae-Young;Lim, Jeong-Hun;Kim, Dong-Hyun
    • Journal of Preventive Medicine and Public Health
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    • v.41 no.5
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    • pp.307-314
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    • 2008
  • Objectives : We conducted an epidemiologic survey to evaluate the effect of the aircraft noise exposure on the health of the residents near the military airbases in Pyeongtaek City. Methods : The evaluation of environmental noise level, questionnaire survey, and health examination were performed for 917 residents. The study population consisted of four groups: subjects who lived in the village close to the fighter airbase (high exposure), subjects who lived along the course of fighters (intermediate exposure), and subjects near a helicopter airbase, and the control group. Results : The prevalence of the aircraft noise related accident and irritable bowel syndrome in the exposure groups were higher than that of the control group. The risks of noise induced hearing loss, hypertension and diabetes mellitus were higher in the exposed groups than in the control group. The prevalence of anxiety disorder and primary insomnia were higher in the exposed groups than in the control group. Prevalence odd ratios of the risk for primary insomnia after adjusting age, sex, agricultural noise, and occupation were 4.03 [95% confidence interval (95% Cl) 1.56-10.47] for the subject near the helicopter airbase, 1.23 (95% Cl 0.40-3.76) for those intermediately exposed to fighter noise, and 4.99 (95% Cl 2.14-11.64) for those highly exposed to fighter noise. Conclusions : The results of the present study suggest that the aircraft noise may have adverse effects on hearing function, cardiovascular health and mental health. Therefore, it seems to be needed to take proper measures including the control of the aircraft noise and the management of the exposed people's health.

Development of a Control Law to Pneumatic Control for an Anti-G Suit (Anti-G 슈트 공압 제어를 위한 제어법칙 개발)

  • Kim, Chong-sup;Hwang, Byung-moon
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.43 no.6
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    • pp.548-556
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    • 2015
  • The highly maneuverable fighter aircraft such as F-22, F-16 and F-15have the high maneuverability to maximize the combat performance, whereas the high maneuver characteristics might degrade the pilot's mission efficiency due to fatigue's increase by exposing him to the high gravity and, in the worst case, the pilot could face GLOC (Gravity-induced Loss Of Consciousness). The advanced aerospace company has applied the various technologies to improve the pilot's tolerance to the gravity acceleration, in order to prevent the pilot from entering the situation of the loss of consciousness. Especially, the Anti-G Suit(AGS) equipment to protect the pilot against the high gravity in flight could improve the mission success rate by decreasing the pilot's fatigue in the combat maneuver as well as prevent the pilot from facing GLOC. In this paper, a control algorithm is developed and verified to provide an optimal air pressure to AGS according to the gravity increase during the high performance maneuver. This result is expected, as the key technology, to contribute to the KF-X(Korean Fighter eXperimental), project in the near future.

Development of Planar Active Electronically Scanned Array(AESA) Radar Prototype for Airborne Fighter (항공기용 평면형 능동 전자주사식 위상 배열(AESA) 레이더 프로토 타입 개발)

  • Chong, Min-Kil;Kim, Dong-Yoon;Kim, Sang-Keun;Chon, Sang-Mi;Na, Hyung-Gi
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.21 no.12
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    • pp.1380-1393
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    • 2010
  • This paper presents a design, fabrication and the test results of planar active electronically scanned array(AESA) radar prototype for airborne fighter applications using transmit/receive(T/R) module hybrid technology. LIG Nex1 developed a AESA radar prototype to obtain key technologies for airborne fighter's radar. The AESA radar prototype consists of a radiating array, T/R modules, a RF manifold, distributed power supplies, beam controllers, compact receivers with ADC(Analog-to-Digital Converter), a liquid-cooling unit, and an appropriate structure. The AESA antenna has a 590 mm-diameter, active-element area capable of containing 536 T/R modules. Each module is located to provide a triangle grid with $14.7\;mm{\times}19.5\;mm$ spacing among T/R modules. The array dissipates 1,554 watts, with a DC input of 2,310 watts when operated at the maximum transmit duty factor. The AESA radar prototype was tested on near-field chamber and the results become equal in expected beam pattern, providing the accurate and flexible control of antenna beam steering and beam shaping.

FS-X 미.일 공동개발 사업 평가

  • Kim, Ho-Sik
    • Defense and Technology
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    • no.4 s.230
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    • pp.30-37
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    • 1998
  • 본 내용은 RAND 연구소에서 발행한 보고서 Troubled Partnership An Assessment of U.S.-Japan Collaboration on the FS-X Fighter의 요약으로 전형적인 미국의 시각에서 사업 위주로 분석하였다. 기 발행된 보고서와 상호 보완 역할을 하여 독자들에게 객관적인 자료를 제공하게 되어 그 의의가 클 것이다. 이보고서는 미국과 일본의 FS-X 전투기 공동 개발에 관한 RAND 연구소의 조사 결과와 평가를 종합한 것이며, 장기간에 걸친 미 항공우주산업 협력 개발사업의 적용과 기술 이전 문제에 초점을 맞추고 있다.

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Airplane mode decoupling using eigenstructure assignment via non-linear optimization (항공기 운동분리의 비선형 최적화를 이용한 고유공간지정법의 응용)

  • 이승재;김유단
    • 제어로봇시스템학회:학술대회논문집
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    • 1993.10a
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    • pp.920-925
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    • 1993
  • For a multi-input, multi-output system, it is widely known that feedback control gain presents extra freedom pole placement problem. An eigenstructure assignment utilizes this freedom for assignment of all or some elements of the closed-loop eigenvectors. In this paper, a nonlinear optimization technique is adopted to obtain a small gain controller that assigns closed-loop eigenvalues and elements of eigenvectors simultaneously. To illustrate the approach, a numerical example of the Airplane mode decoupling using an advanced fighter is shown.

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Innovative Technologies for Tactical Combat Aircraft Powerplants (전술전투기용 추진기관의 혁신 기술)

  • Lee, Gi-Yeong;Gang, Su-Jun
    • The Journal of Aerospace Industry
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    • s.45
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    • pp.67-81
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    • 1998
  • With projections into the future advanced Korea fighter development, the trend of tactical combat aircraft powerplants technique development over the past decade is presented. Ti was particularly focused on current innovative powerplants technologies such as lower density stronger materials and turbomachniery aerodynamics. With reviewing the status of aircraft powerplants which are currently underdeveloped next generation combat aircraft, it shows some core techniques that are needed for developing Korean type combat aircraft.

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A Flow Analysis of Vectored Thrust Nozzle Using Incompressible Navier-Stokes Solver (비압축성 Navier-Stokes 방정식을 이용한 추력 편향 노즐 해석(원통에서 사각형으로 변환하는 내부 흐름을 중심으로))

  • Shin Dae-Yong;Yoon Yong-Hyun
    • 한국전산유체공학회:학술대회논문집
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    • 1997.10a
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    • pp.66-72
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    • 1997
  • Circular-to-rectangular transition ducts are used as exhaust components of high performance fighter aircraft with vectored thrust nozzles. Three-dimensional incompressible Navier-Stokes solver is used to analyze the transition duct. Cross sections of transition duct are defined by superelliptic equation. The grid system is generated by Non-Uniform Rational B-Spline, after generating surface grid by blending the cross sections. Good agreement between the results of the computational simulation and the experimental data is observed.

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