• Title/Summary/Keyword: Radar Position

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Position Estimation of a Missile Using Three High-Resolution Range Profiles (3개의 고 분해능 거리 프로파일을 이용한 유도탄의 위치 추정)

  • Yang, Jae-Won;Ryu, Chung-Ho;Lee, Dong-Ju
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.29 no.7
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    • pp.532-539
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    • 2018
  • A position estimation technique is presented for a missile using high-resolution range profiles obtained by three wideband radars. Radar measures a target range using a reflected signal from the surface of a missile. However, it is difficult to obtain the range between the radar and the origin of the missile. For this reason, the interior angle between the moving missile and tracking radar is calculated, and a compensated range between surface of the missile and its origin is added to the tracking range of the radar. Therefore, position estimation of a missile can be achieved by using three total ranges from each radar to the origin of the missile. To verify the position estimation of the missile, electromagnetic numerical analysis software was used to prove the compensated range according to the flight position. Moreover, a wideband radar operating at 500-MHz bandwidth was applied, and its range profile was used for the position estimation of a missile.

Method on Radar deployment for Ballistic Missile Detection Probability Improvement (탄도미사일 탐지확률 향상을 위한 레이더 배치 방안)

  • Park, Tae-yong;Lim, Jae-sung
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.20 no.3
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    • pp.669-676
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    • 2016
  • North Korea has various ballistic missiles from short range to long range such as inter continental ballistic missiles. Short range ballistic missiles such as SCUD series are threatening to Korea peninsula. Therefore Korea is constructing various missile defense systems to protect country. Parameters influencing the received power from the target to the radar are transmitting power, antenna gain, carrier frequency, RCS(Radar Cross Section) of target and distance from radar to target. Especially, RCS and distance from target are not radar performance defined parameters but external parameters. Therefore radar deployment position that large RCS can be observed and target to radar distance should be considered in parallel to improve target detection probability. In this paper, RCS pattern of SCUD-B ballistic missile is calculated, received power is analyzed based on radar deployment position during ballistic missile trajectory and methode for optimum radar deployment position to improve target detection probability is suggested.

A Study on Radar Received Power based on Target Observing Position (표적 관측 위치에 따른 레이더 수신 전력에 관한 연구)

  • Park, Tae-Yong;Lee, Yura
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.18 no.12
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    • pp.3063-3068
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    • 2014
  • Since the RCS(Radar Cross Section) of target is important factor to determine radar performance, it is important to locate radar where large RCS is observed. However, the distance between the target and the radar is an important factor of the received power, as well as RCS. In this paper, it is calculated that received power from ballistic missile to radar based on different observed position and it is studied that to place radar for high detection efficiency.

KSR-III 궤도데이터 취득시스템 개발

  • Lee, Sang-Rae;Lee, Soo-Jin;Kim, Jun-Kyu;Lee, Jae-Deuk
    • Aerospace Engineering and Technology
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    • v.2 no.1
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    • pp.133-139
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    • 2003
  • Position and trajectory data in-flight rocket are important informations to determine flight safety of rocket. In general tracking system, radar and transponder are used to acquire position information. Rocket position and trajectory can be determined by RF communication between ground station and in-flight rocket, and antenna position date. In this paper, it explains the ranging system which is low resolution rather than radar system but system configuration is simple. Therefore this system is useful for experimental flight vehicle.

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Real-time position tracking of traffic ships by ARPA radar and AIS in Busan Harbor, Korea (부산항에서 ARPA 레이더와 AIS에 의한 통한선박의 실시간 위치추적)

  • Lee, Dae-Jae
    • Journal of the Korean Society of Fisheries and Ocean Technology
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    • v.44 no.3
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    • pp.229-238
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    • 2008
  • This paper describes on the consolidation of AIS and ARPA radar positions by comparing the AIS and ARPA radar information for the tracked ship targets using a PC-based ECDIS in Busan harbor, Korea. The information of AIS and ARPA radar target was acquired independently, and the tracking parameters such as ship's position, COG, SOG, gyro heading, rate of turn, CPA, TCPA, ship s name and MMSI etc. were displayed automatically on the chart of a PC-based ECDIS with radar overlay and ARPA tracking. The ARPA tracking information obtained from the observed radar images of the target ship was compared with the AIS information received from the same vessel to investigate the difference in the position and movement behavior between AIS and ARPA tracked target ships. For the ARPA radar and AIS targets to be consolidated, the differences in range, speed, course, bearing and distance between their targets were estimated to obtain a clear standards for the consolidation of ARPA radar and AIS targets. The average differences between their ranges, their speeds and their courses were 2.06% of the average range, -0.11 knots with the averaged SOG of 11.62 knots, and $0.02^{\circ}$ with the averaged COG of $37.2^{\circ}$, respectively. The average differences between their bearings and between their positions were $-1.29^{\circ}$ and 68.8m, respectively. From these results, we concluded that if the ROT, COG, SOG, and HDG informations are correct, the AIS system can be improved the prediction of a target ship's path and the OOW(Officer of Watch) s ability to anticipate a traffic situation more accurately.

3단형 과학관측로켓용 탑재 트랜스폰더 시스템 개발

  • Kim, Sung-Wan;Lee, Soo-Jin;Kim, Joo-Nyun;Ma, Keun-Su;Kim, Jun-Kyu
    • Aerospace Engineering and Technology
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    • v.1 no.1
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    • pp.135-140
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    • 2002
  • The position and trajectory of in-flight rocket are important informations to determine the flight safety of rocket. In general tracking system, radar and transponder are used to acquire position information. Rocket position and trajectory can be determined by using RF communication between ground station and in-flight rocket and antenna position data. Onboard transponder system is composed of RF receiving part, RF transmitting one, decoder and single TX/ RX antenna. Therefore circulator is necessary for minimizing RF signal interference. In this paper, the radar transponder system was developed to track the trajectory and position of KSR-Ⅲ by using radar.

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An Analysis of 2D Positional Accuracy of Human Bodies Detection Using the Movement of Mono-UWB Radar

  • Kiasari, Mohammad Ahangar;Na, Seung You;Kim, Jin Young
    • Journal of Sensor Science and Technology
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    • v.23 no.3
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    • pp.149-157
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    • 2014
  • This paper considers the ability of counting and positioning multi-targets by using a mobile UWB radar device. After a background subtraction process, distinguishing between clutters and human body signals, the position of targets will be computed using weighted Gaussian mixture methods. While computer vision offers many advantages, it has limited performance in poor visibility conditions (e.g., at night, haze, fog or smoke). UWB radar can provide a complementary technology for detecting and tracking humans, particularly in poor visibility or through-wall conditions. As we know, for 2D measurement, one method is the use of at least two receiver antennas. Another method is the use of one mobile radar receiver. This paper tried to investigate the position detection of the stationary human body using the movement of one UWB radar module.

A study of effective filter algorithms for multi-target tracking (다중표적추적을 위한 효과적인 필터 알고리듬에 대한 연구)

  • 이동관;송택렬
    • 제어로봇시스템학회:학술대회논문집
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    • 2000.10a
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    • pp.99-99
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    • 2000
  • An effect ive filter algorithm that can manage radar beam pointing efficiently is needed to track multi-target in the air. For effective beam management the filter has lobe good enough to predict future position of target and based on this filter output radar beam is control led to point toward the predicted target position in the air. In this paper, we investigate the ${\alpha}$-${\beta}$ filter known for its brief filter structure with the steady-state Kalman filter gain, the ruv filter, and the coordinate-transformed filter that can decouple the measurement noise variance.

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A POSITION TRACKING ALGORITHM WITH RADAR MEASUREMENT

  • Lim You-Chol;Ma Keun-Su;Lee Jae-Deuk
    • Bulletin of the Korean Space Science Society
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    • 2004.10b
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    • pp.332-336
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    • 2004
  • This paper describes the remote tracking algorithm using measurements (azimuth, elevation, and slant range) of the radar ground station. Kalman filter model for noise reduction of the measured information is first derived by linearizing with respect to angle, angular rate, range, and range rate. And then a tracking algorithm is introduced to calculate the position of the vehicle during in-flight. The simulation results show that the algorithm is practical and effective enough tracking position of the vehicle in considerably less error.

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Quantitative Analysis of Automotive Radar-based Perception Algorithm for Autonomous Driving (자율주행을 위한 레이더 기반 인지 알고리즘의 정량적 분석)

  • Lee, Hojoon;Chae, HeungSeok;Seo, Hotae;Yi, Kyongsu
    • Journal of Auto-vehicle Safety Association
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    • v.10 no.2
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    • pp.29-35
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    • 2018
  • This paper presents a quantitative evaluation method and result of moving vehicle perception using automotive radar. It is also important to analyze the accuracy of the perception algorithm quantitatively as well as to accurately percept nearby moving vehicles for safe and efficient autonomous driving. In this study, accuracy of the automotive radar-based perception algorithm which is developed based on interacting multiple model (IMM) has been verified via vehicle tests on real roads. In order to obtain experimental data for quantitative evaluation, Long Range Radar (LRR) has been mounted on the front of the ego vehicle and Short Range Radar (SRR) has been mounted on the rear side of both sides. RT-range has been installed on the ego vehicle and the target vehicle to simultaneously collect reference data on the states of the two vehicles. The experimental data is acquired in various relative positions and velocity, and the accuracy of the algorithm has been analyzed according to relative position and velocity. Quantitative analysis is conducted on relative position, relative heading angle, absolute velocity, and yaw rate of each vehicle.