• Title/Summary/Keyword: Aircraft Radar

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Integrated Operation Concept of Terminal Control Areas for Efficient Use of Airspace (공역 효율화를 위한 접근관제구역 통합운용 개념 연구)

  • Chang, Man-Heui;Jo, Sanghoon;Lee, Eunju;Kang, Ja-Young;Yoo, Byeong-Seon
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.22 no.1
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    • pp.108-113
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    • 2014
  • Recently increase in the number of aircraft caused the air traffic congestion and flight delays. If timely action to reform the air traffic system is not taken, these may result in added economic impact. As a result, the air traffic management should be changed in an innovative manner to modernize the existing air traffic control environment. This paper reviews the trends of airspace reforms such as integration of terminal control areas and flexible use of airspace introduced by foreign countries and compares their merits and demerits in order to provide a judgement to adopt the concept in domestic airspace in the future.

COMBINED ACTIVE AND PASSIVE REMOTE SENSING OF HURRICANE OCEAN WINDS

  • Yueh, Simon H.
    • Proceedings of the KSRS Conference
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    • v.1
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    • pp.142-145
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    • 2006
  • The synergism of active and passive microwave techniques for hurricane ocean wind remote sensing is explored. We performed the analysis of Windsat data for Atlantic hurricanes in 2003-2005. The polarimetric third Stokes parameter observations from the Windsat 10, 18 and 37 GHz channels were collocated with the ocean surface winds from the Holland wind model, the NOAA HWind wind vectors and the Global Data Assimilation System (GDAS) operated by the National Center for Environmental Prediction (NCEP). The collocated data were binned as a function of wind speed and wind direction, and were expanded by sinusoidal series of the relative azimuth angles between wind and observation directions. The coefficients of the sinusoidal series, corrected for atmospheric attenuation, have been used to develop an empirical geophysical model function (GMF). The Windsat GMF for extreme high wind compares very well with the aircraft radiometer and radar measurements.

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Bandpass Antenna-Filter-Antenna Arrays for Millimeter-Wave Filtering Applications

  • Kaouach, Hamza;Kabashi, Amar;Simsim, Mohammed T.
    • Journal of electromagnetic engineering and science
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    • v.15 no.4
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    • pp.206-212
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    • 2015
  • This paper introduces new wideband antenna-filter-antenna (AFA) uniform arrays that can be utilized as frequency selective surfaces (FSS) with low loss and sharp roll-off response, which are highly desirable characteristics for millimeter wave applications. The design adopts a simple 3-layer single polarization structure consisting of two patch antennas and a resonator. Both simulations and measurements are used to characterize the performances of the proposed design. Overall results show 18.5% 10-dB bandwidth. For the targeted band the insertion loss is less than 0.2 dB. Possible applications include quasi-optical amps, grid mixers and radomes for aircraft radar antennas.

AN INTEGRATED SYSTEM FOR COMPUTATIONAL AERODYNAMIC, STRUCTURAL AND RF STEALTH ANALYSIS (공력-구조-RF 스텔스 통합 전산해석 시스템 연구)

  • Park, G.R.;Yang, Y.R.;Jung, S.K.;Myong, R.S.;Cho, T.H.
    • 한국전산유체공학회:학술대회논문집
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    • 2010.05a
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    • pp.78-82
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    • 2010
  • An integrated multi-disciplinary design system plays a critical role in the preliminary design of an aircraft. In this paper such system is developed for the multi-disciplinary computation and design; aerodynamics elasticity, and radio frequency stealth. Common data base of geometry and structured grids is generated and used for aerodynamic, structural and eletromagnetics analysis. The Navier-Stokes CFD, FEM, and CEM technique are used for aerodynamic, structural, and RF stealth computations respectively.

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Microstrip Antenna for SAR Applications with Microwave Composite Laminates and Honeycomb Cores (복합재료 하니콤 샌드위치 판넬을 이용한 SAR 시스템용 마이크로스트립 안테나 개발)

  • 유치상;이라미;황운봉;박현철;박위상
    • Proceedings of the Korean Society For Composite Materials Conference
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    • 2000.11a
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    • pp.195-198
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    • 2000
  • Microstrip antenna for SAR applications is designed with microwave composite laminates and Nomex honeycomb cores, which becomes an aircraft's structural panel. This study demonstrated fabrication, design procedures and structural and electrical performances of complex antenna system presented. For validating structural rigidity, 3-point bending test is performed, and simulation results for the complex antenna array are compared with measurements for its electrical performance. The results show that this antenna system can be applied in dual polarized synthetic aperture radar and has a good flexural stiffness with comparison of previous sandwich constructions.

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The Design of 35GHz Multi-Purpose Navigation Radar For Lower Speed Aircraft (저속 항공기를 위한 35GHz 다기능 항행 레이다 설계)

  • Mun, Sang-Man;Kim, Hyeon-Gyeong;Lee, Sang-Jong;Kim, In-Gyu;Kim, Tae-Sik;Lee, Hae-Chang
    • 한국항공운항학회:학술대회논문집
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    • 2004.11a
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    • pp.247-252
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    • 2004
  • 민항기나 군용항공기의 경우 대부분 항행 안전성을 확보하기 위해 다양한 기능을 수행하는 레이다가 부착되어 있으나, 소형항공기 및 저가의 헬기의 경우 무게, 비용 등의 제약으로 항행 안전을 확보할 수 있는 레이다가 장착되어 있지 않는 실정이다. 따라서 본 연구에서는 민항기 및 군용 항공기뿐만이 아니라 헬기 및 소형항공기에 장착하여 충돌감지, 이착륙보조, 기상관측 등의 기능을 수행할 수 있는 레이다로 35GHz 밀리미터 대역의 항공기 탑재형 레이다의 적용에 대한 제반 요건과 필요성에 대한 연구를 수행하였다. 그리고 제안된 레이다를 이용하면, 저속 항공기 및 헬기에서는 치명적인 사고를 유발시킬 수 있는 전력선 탐지가 가능함을 확인함으로써, 제안된 레이다가 항행 안전성을 높일 수 있음을 보임으로써 밀리미터 대역 레이다의 적용이 가능함을 확인하였다.

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A Review on Monitoring Mt. Baekdu Volcano Using Space-based Remote Sensing Observations (인공위성 원격탐사를 이용한 백두산 화산 감시 연구 리뷰)

  • Hong, Sang-Hoon;Jang, Min-Jung;Jung, Seong-Woo;Park, Seo-Woo
    • Korean Journal of Remote Sensing
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    • v.34 no.6_4
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    • pp.1503-1517
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    • 2018
  • Mt. Baekdu is a stratovolcano located at the border between China and North Korea and is known to have formed through its differentiation stage after the Oligocene epoch in the Cenozoic era. There has been a growing interest in the magma re-activity of Mt. Baekdu volcano since 2010. Several research projects have been conducted by government such as Korea Meteorological Administration and Korea Institute of Geoscience and Mineral Resources. Because, however, the Mt. Baekdu volcano is located far from South Korea, it is quite difficult to collect in-situ observations by terrestrial equipment. Remote sensing is a science to analyze and interpret information without direct physical contact with a target object. Various types of platform such as automobile, unmanned aerial vehicle, aircraft and satellite can be used for carrying a payload. In the past several decades, numerous volcanic studies have been conducted by remotely sensed observations using wide spectrum of wavelength channels in electromagnetic waves. In particular, radar remote sensing has been widely used for volcano monitoring in that microwave channel can gather surface's information without less limitation like day and night or weather condition. Radar interferometric technique which utilized phase information of radar signal enables to estimate surface displacement such as volcano, earthquake, ground subsidence or glacial movement, etc. In 2018, long-term research project for collaborative observation for Mt. Baekdu volcano between Korea and China were selected by Korea government. A volcanic specialized research center has been established by the selected project. The purpose of this paper is to introduce about remote sensing techniques for volcano monitoring and to review selected studies with remote sensing techniques to monitor Mt. Baekdu volcano. The acquisition status of the archived observations of six synthetic aperture radar satellites which are in orbit now was investigated for application of radar interferometry to monitor Mt. Baekdu volcano. We will conduct a time-series analysis using collected synthetic aperture radar images.

A Study on Reliability Improvement of RALT for KUH through Fault Analysis (한국형기동헬기 레이더고도계의 결함분석을 통한 신뢰성 향상에 관한 연구)

  • Jun, Byung Kyu;Kim, Young Mok;Chang, Joong Jin;Kim, Chang Young;Hwang, Gil Won
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.42 no.5
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    • pp.406-414
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    • 2014
  • In this paper, it is introduced characteristics of FMCW-type Radar Altimeter for KUH, and its defects occurred during ground/flight test in initial product phase. In addition, it is also described 'data/control flow model' based fault analysis results of S/W and processes of verifying improvement design through flight test as well as aircraft system integration test called MEP SIL. As a result of design improvement and verification, it is validated that settling the defects and improving not only safety but also capability of the KUH.

Operational Concept Design and Verification for Airborne SAR System (항공탑재 SAR 시스템 운용개념 설계 및 검증)

  • Lee, Hyon-Ik;Kim, Se-Young;Jeon, Byeong-Tae;Sung, Jin-Bong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.41 no.7
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    • pp.588-595
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    • 2013
  • Airborne SAR system is the imaging Radar system that is loaded on a manned or unmanned aircraft, which is in charge of high quality image acquisition and moving target detection. This paper describes the operational requirements for the Airborne SAR system and suggests the operational concept to satisfy the requirements. To be specific, it describes the interface with airborne system, state definition and transition, operation mode based on mission definition file, fault management, and data storing and transmission concept. Finally, it gives the ground test results to verify the SAR system operational concept.

The Deviation Distribution of Target on the ILS Final Approach Segment Using ADS-B Message (ADS-B 신호를 이용한 ILS 최종접근 구간의 항공기 항적 이격 분포 도출)

  • Ku, SungKwan;Lee, Young-Jong;Shin, DaiWon
    • Journal of Advanced Navigation Technology
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    • v.19 no.5
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    • pp.403-410
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    • 2015
  • ADS-B can provide high accurate position information and faster update rate than Radar system and it is a technique that can supplement or replace the Radar. Recently ADS-B has been applied to the actual aircraft operation because to increase air transportation traffic and required to high accurate surveillance. In this study, we surveyed analysis of position deviation distribution analysis and received actual ADS-B trajectory data for conformed precise surveillance on the near airport area using ADS-B message. For that, we received the precision instrument approach ADS-B trajectory data using instrument landing system, and can analyse about target deviation distribution on the final approach segment about precision instrument approach. The result of analysis is mean distance of target deviation -0.04 m and standard deviation 6.71 m on between ADS-B target and extended runway centerline. Also that is to conformed the ADS-B message trajectory available to provide relatively exact surveillance information.