• 제목/요약/키워드: Radar System Design

검색결과 352건 처리시간 0.03초

전차 탑재 L-밴드 펄수 도플러 레이더 설계 및 제작 (L-band Pulsed Doppler Radar Development for Main Battle Tank)

  • 박규철;하종수
    • 한국전자파학회논문지
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    • 제20권6호
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    • pp.580-588
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    • 2009
  • 전차 탑재 레이더는 기상에 관계없이 전천후로 대전차 미사일을 탐지하는 능동 방호 장치의 필수적인 센서이다. 본 논문에서는 전차 탑재 레이더의 설계, 제작 및 시험 결과를 제시한다. 레이더 시스템은 안테나부, 송수신부, 신호처리부의 3개의 LRU로 구성되며, 개발 기술은 패치 안테나, SSPA 송신기, coherent I/Q detector, DSP기반 도플러 FFT 필터, 적응 CFAR, TWS 추적기 및 위협 판단을 포함한다. 개발된 레이더 시스템의 설계 성능은 고정 및 기동 시험을 통하여 확인한다.

헬기탑재 다중모드 레이다 시스템 모델 설계 (Multi-Mode Radar System Model Design for Helicopter)

  • 곽영길;배재훈
    • 한국전자파학회:학술대회논문집
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    • 한국전자파학회 2003년도 종합학술발표회 논문집 Vol.13 No.1
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    • pp.208-212
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    • 2003
  • An airborne radar is an essential aviation electronic system of the helicopter to perform various missions in all-weather environments. This paper presents the conceptual design results of the multi-mode pulsed Doppler radar system testbed model for helicopter. Due to the inherent flight nature of the hovering vehicle which is flying in low-altitude and low speed, as well as rapid maneuvering, the moving clutters from the platform should be suppressed by using a special MTD (Moving Target Detector) processing. For the multi-mode radar system model design, the flight parameters of the moving helicopter platform were assumed: altitude of 3 Km, average cruising velocity of 150knots. The multi-mode operation capability was applied such as short-range, medium-range, and long-range depending on the mission of the vehicle. The nominal detection ranges is 30 Km for the testbed experimental model, but can be expanded up to 75 Km for the long range weather mode. The detection probability of each mode is also compared in terms of the signal-to noise ratio of each mode, and the designed radar system specifications ate provided as a design results.

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항공기용 전파흡수 구조 연구 (A Study on Radar Absorbing Structure for Aircraft)

  • 한원재;장병욱;박정선
    • 항공우주시스템공학회지
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    • 제4권3호
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    • pp.24-28
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    • 2010
  • The purpose of this study is to define available microwave absorbing structure for aircraft from in the X-band(8.2~12.4GHz) frequencies. The electromagnetic wave absorption or shielding techniques is an important issue not only for military purpose but also for commercial purposes. Aircraft Radar Absorbing Structure(RAS) is absorbed or scattered propagation waves from the enemy radar. There are absorbing technologies at shaping design techniques and using Radar Absorbing Materials(RAM). RAM is more important because shaping design can't include perfect radar absorbing performance. In this study, based on material properties was introduced RAM and to analyze the each characteristics. Finally, we comparison appropriate RAM for aircraft.

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Ground Penetrating Radar를 사용한 지하설비 탐사에 관한 연구 (Exploration of Buried Facilities by GPR)

  • 손수국;전경수
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2001년도 합동 추계학술대회 논문집 정보 및 제어부문
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    • pp.30-33
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    • 2001
  • This paper discusses the system design of a synthetic aperture radar system based on a pulse-echo radar. The design consists of an ultra-wide bandwidth antenna, an amplitude modulation, timing stabilities, and high speed a/d conversions with an equivalent-time sampling. Experiment results show that GPR(Ground Penetrating Radar) can be used to explore buried electric facilities.

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Robust Transmission Waveform Design for Distributed Multiple-Radar Systems Based on Low Probability of Intercept

  • Shi, Chenguang;Wang, Fei;Sellathurai, Mathini;Zhou, Jianjiang;Zhang, Huan
    • ETRI Journal
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    • 제38권1호
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    • pp.70-80
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    • 2016
  • This paper addresses the problem of robust waveform design for distributed multiple-radar systems (DMRSs) based on low probability of intercept (LPI), where signal-to-interference-plus-noise ratio (SINR) and mutual information (MI) are utilized as the metrics for target detection and information extraction, respectively. Recognizing that a precise characterization of a target spectrum is impossible to capture in practice, we consider that a target spectrum lies in an uncertainty class bounded by known upper and lower bounds. Based on this model, robust waveform design approaches for the DMRS are developed based on LPI-SINR and LPI-MI criteria, where the total transmitting energy is minimized for a given system performance. Numerical results show the effectiveness of the proposed approaches.

파라미터 불확실성 및 시간지연을 갖는 레이더 김벌 안정화 시스템의 지연종속 퍼지 H 제에 (Delay Dependent Fuzzy H Control of Radar Gimbal Stabilization System with Parameter Uncertainty and Time Delay)

  • 김태식;이해창;이갑래
    • 제어로봇시스템학회논문지
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    • 제11권11호
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    • pp.920-929
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    • 2005
  • This paper presents controller design method for nonlinear radar gimbal system with parameter uncertainty and time delay. In order to consider nonlinearity of gimbal bearing frictional torque, we firstly represent fuzzy model for the nonlinear gimbal system, which is achieved by fuzzy combination of linear models through nonlinear fuzzy membership functions. And secondly we propose a delay dependent fuzzy $H_\infty$ controller design method for the delayed fuzzy model with parameter uncertainty and design radar gimbal controller. The designed controller stabilize gimbal system and guarantee $H_\infty$ performance. A computer simulation is given to illustrate stabilized control performances of the designed controller.

비행체 탑재 펄스 도플러 레이다 시험모델 개발 (Airborne Pulsed Doppler Radar Development)

  • 곽영길;최민수;배재훈;전인평;양주열
    • 한국항행학회논문지
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    • 제10권2호
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    • pp.173-180
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    • 2006
  • 비행체 탑재 레이다는 기상에 관계없이 전천후로 비행체의 안전항행, 임무감시, 사격통제, 충돌회피, 이착륙 등 비행에 필수적인 항공장치이다. 본 논문에서는 비행체 탑재 다중 모드 펄스 도플러 레이다 시험 모델의 설계, 제작 및 비행시험 결과를 제시한다. 레이다 시스템은 안테나부, 송수신부, 신호처리부와 전시부의 4-LRU(Line Replacement Unit)로 구성되며, 개발기술은 평판 슬롯 배열 안테나, TWTA 송신기, coherent I/Q detector, 디지털 펄스 압축, 도플러 FFT 필터를 기반으로 한 DSP, 적응 CFAR, TWS 추적 처리기, 비행정보 IMU 및 도플러 추정보상 기법을 포함한다. 개발된 레이다 시스템의 설계 성능은 다양한 헬기탑재 비행시험을 통하여 기능 및 성능을 확인하였다.

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Design of Passive-Type Radar Reflector

  • Yim, Jeong-Bin;Kim, Woo-Suk
    • 한국항해항만학회지
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    • 제27권3호
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    • pp.267-272
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    • 2003
  • This paper describes design method of Passive-type Radar Reflector (PRR) which is to provide the requirement of newly revised 2000 SOLAS regulations on the Radar Reflector. The main target of this work is to find the optimum shape of a radar target having large Radar Cross Section (RCS). Through the RCS analysis based on the theoretical approach, two kinds of PRR models, RRR-F model for use in fisheries and PRR-S model for use in small sized ship, are designed and discussed their RCS performance. RCS measurement tests for the various sized samples are carried out in an anechoic chamber. As evaluation results it was clearly shown that the conventional sphere-type shows optimum shape in case of PRR-S, while the cylinder-type which consists of large sized corner clusters or zig-zag flat plats gives best performance in case of PRR-F.

Design and implementation of signal processing system for airborne active homing radar

  • Lee, Young-Sung;Kim, Doh-Hyun;Kim, Lee-Han;Kim, Young-Chae
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2001년도 ICCAS
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    • pp.158.2-158
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    • 2001
  • This paper introduces the design and implementation of a signal processing system for an airborne active homing radar system. This airborne active homing radar system uses the pulse Doppler radar of high PRF (Pulse Repetition Frequency) for computation of exact relative velocity of the target. This system carries out two operations mainly. The first is to transmit and receive microwave signal through the antenna. The second is to calculate the relative velocity of the target taking advantage of the Doppler frequency signal reflected from the target and detect the angle error between a target and an antenna LOS (Line Of Sight) to make the antenna direction coincident with the target. The signal processing system has a role of the latter.

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A Study on Efficient Design of Surveillance RADAR Interface Control Unit in Naval Combat System

  • Dong-Kwan Kim;Dong-Han Jung;Won-Seok Jang;Young-San Kim;Hyo-Jo Lee
    • 한국컴퓨터정보학회논문지
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    • 제28권11호
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    • pp.125-134
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    • 2023
  • 본 논문은 함정 전투체계에서 효율적인 탐색레이더 연동단 설계 방법을 제안한다. 제안된 탐색 레이더 연동단은 함정 전투체계 소프트웨어에서 공용화 모듈(Module)을 표준화한 구조를 적용하였다. 링크(Link)별 오류탐지 기능을 구현하여 링크 단절시 링크 단절에 대한 인지 속도를 높였다. 또한 HCI(Human-Computer Interaction)를 위해 주기적으로 전송하던 메시지를 데이터그램(Datagram)의 변화가 있을 때만 송신하여 콘솔(Console)의 처리 부하를 줄일 수 있다. 특히 제안 방법은 함정에서 저가형 상용 탐색레이더 채택 등으로 프로세싱(Processing) 능력이 뛰어나지 못한 경우 사격에 대한 명중 확인 및 영점 조절과 관련하여 워터폴 스코프(Waterfall Scope)와 시간 제한 물기둥 인지 방법으로 탐색레이더의 기능을 보완해줄 수 있다. 이를 통해 운용자의 사격 명중 판단이 용이해지고, 오인지 확률을 줄일 수 있으며, 탐색레이더의 가용자원을 추가로 확보할 수 있다.