• Title/Summary/Keyword: Radar altimeter

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Examination of Altimeter Wave Data in the Sea Around Ieodo Ocean Research Station (이어도 해양과학기지 인근해역에서의 고도계 파고 자료 검증)

  • Kim, Tae-Rim
    • Korean Journal of Remote Sensing
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    • v.28 no.1
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    • pp.95-100
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    • 2012
  • Big swell is often generated offshore and damages the coasts after travelling long distance. In order to prevent coastal damages, wave measurements should be performed offshore as well as coastal waters around Korea. However, in-situ wave measurements are difficult because of high expense of instruments and high risk of operation. Satellite wave measurements using altimeter make it possible to get wave information from the sea difficult to execute field measurements such as the center of the East Sea or exclusive territorial waters. In order to use wave information from the satellite altimeter, it is important to verify altimeter wave data with in-situ data. This paper examines significant wave height data observed by ENVISAT altimeter by comparing wave data observed at Ieodo station.

Distribution of Antarctic Sea Ice from Satellite Altimetry in the Weddell Sea: Preliminary Results

  • Kim, Jeong-Woo;Hong, Sung-Min;Hwang, Jong-Sun;Yoon, Ho-Il;Lee, Bang-Yong;Kim, Yea-Dong
    • Ocean and Polar Research
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    • v.24 no.3
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    • pp.255-261
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    • 2002
  • We investigated the distribution of sea ice using Topex/Poseidon (T/P) and ERS-1 .ada. altimeter data in the northwest Weddell Sea, Antarctica, between the area $45-75^{\circ}W\;and\;55-66^{\circ}S$. Using the Geo_Bad_1 flag of the Merged GDR of the T/P, we classified the surface into ocean, land, and sea. Total 257 cycles of altimeter measurements between Oct. 1992 and Sep. 1999 (for nearly 2570 days) were used to analyze the distribution of the Antarctic sea ice. We then calculated the surface area of ice coverage using SUTM20 map projection to monitor the periodic variations. Each year, the maximum and minimum coverage of the sea ice were found in late August and February in the study area, respectively. We also studied the sea ice distribution using ERS-1 altimeter data between $45-75^{\circ}W\;and\;55-81.5^{\circ}S$ to compare with the T/P Using the Valid/Invalid flag of the Ocean Product, we analyzed the sea ice distribution between March and August of 1995, which showed very good coherence with the T/P measurements. Our preliminary results showed that the altimeter measurements can be effectively used to monitor the distribution of the sea ice in the polar region. However, the size of radar footprint, typically 2-6km depending on the roughness of the sea surface, may be too big to monitor the sharp boundary between ice and water/land. If more other altimeter mission data with dense coverage such as Geosat GM are analyzed together, this limitation can be significantly improved. If we also combine other microwave remote sensing data such as radiometer, and SSM/I, the result will be significantly enhanced.

Clutter Modeling for HILS (HILS를 위한 클러터 모델링)

  • 최승호
    • Proceedings of the Korea Society for Simulation Conference
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    • 1999.04a
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    • pp.26-31
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    • 1999
  • As a part of work to simulate electromagnetic environments for Hareware-In-the-Loop Simulation, clutter signals of pulsed dopplar radar(altimeter) and CW radar are modeled as numerical expressions for various parameters. The simulated results show that this method is applicable to simulate complex electromagnetic environments.

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Sea Ice Detection using Microwave Remote Sensing Techniques in the Weddell Sea, Antarctica (마이크로웨이브 원격탐사를 이용한 남극 웨델해 해빙 관측)

  • 황종선;이방용;심재설;홍성민;윤호일;권태영;민경덕;김정우
    • Economic and Environmental Geology
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    • v.36 no.2
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    • pp.141-148
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    • 2003
  • We investigated the distribution of sea ice using various microwave remote sensing techniques including radar altimeter, radiometer, and scatterometer data in the part of Drake passage, Antarctica, between the area 45$^{\circ}$-75$^{\circ}$W and 55$^{\circ}$-66$^{\circ}$S. Topex/poseidon radar altimeter data were used to analyze the monthly distribution of sea ice surface area between 1992 and 1999 by using Geo_bad_1 flag or MGDR. From satellite radiometer measurements of DMSP's SSM/I, sea ice concentration was extracted during the period from 1993 to 1996. To select a value of ice concentration, normally ranging from 0 to 100%, that can be used as a critical value of judging the existence for ice, sea ice areas estimated from various ice concentrations of radiometer measurements were correlated with the area estimated from the radar altimeter measurements. As a result, 20% of ice concentration was selected, and, then this value was used to integrate radiometer data with radar altimeter and ERS-1/2 scatterometer data. To indirectly verify the result, the last 20 year's sea ice concentration was correlated with surface temperature data near Esper-anza Observation Station. The two data showed a high correlation coefficient of 0.86. The amount of sea ice and temperature variation were found to be closely related in the study area, and this indirectly verifies the result of this study. We provided a method to judge the existence of sea ice from ice concentration of satellite radiometer data and suggested a method to monitor more detailed temporal and spatial variation of sea ice distribution by integra-tion of various microwave remote sensing techniques.

W-Band Radar Altimeter for Drones (드론용 W-대역 레이다 고도계)

  • Lee, Yong-Seok;Lee, Gwon-Hak;Kim, Jun-Seong;Park, Jae-Hyun;Kim, Byung-Sung;Song, Reem
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.30 no.4
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    • pp.314-319
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    • 2019
  • In this study, we propose a W-band frequency modulated continuous wave(FMCW) radar altimeter that can measure the altitude based on the frequency differences of transmitted and received signals. This W-band FMCW system is powered by an altitude control algorithm, which we propose to help prevent collisions of drones with obstacles in real deployment by measuring the relative altitude. It is shown that this algorithm enables the drone to be positioned within a 3 % error of altitude from the desired input height. The chip used in the W-band transmitter and receiver was fabricated using a 65-nm CMOS process, and a horn antenna was directly fed by incorporating an embedded waveguide feeder into the chip. The clutter spectra observed in terrains including soil, grass, and calm lake water were measured and compared, confirming the reflectivity characteristics of various surfaces of different water contents.

A performance analysis of terrain-aided navigation(TAN) algorithms using interferometric radar altimeter (간섭계 레이더 고도계를 활용한 지형참조항법의 성능 분석)

  • Jeong, Seung-Hwan;Yoon, Ju-Hong;Park, Min-Gyu;Kim, Dae-Young;Sung, Chang-Ki;Kim, Hyun-Suk;Kim, Yoon-Hyung;Kwak, Hee-Jun;Sun, Woong;Yoon, Kuk-Jin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.40 no.4
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    • pp.285-291
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    • 2012
  • The paper experimentally verifies the performance of Terrain-Aided Navigation (TAN) using an interferometric radio altimeter, which is recently used due to its accuracy. First, we propose a TAN system that utilizes an interferometric radio altimeter as a measurement system. Second, we implement extended Kalman filter, unscented Kalman filter, and particle filter to evaluate the performance of TAN according to the selection of filters and the difference of environments.

Performance Analysis of Interferometric Radar Altimeter by Terrain Type for Estimating Reliability of Terrain Referenced Navigation (지형대조항법의 신뢰성 추정을 위한 간섭계 레이더 고도계의 지형 유형별 성능 분석)

  • Ha, Jong Soo;Lee, Han Jin;Lee, Soo Ji;Hong, Sung Yong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.50 no.2
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    • pp.83-92
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    • 2022
  • This paper analyzes the performance of the IRA(Interferometric Radar Altimeter) by terrain type for estimating reliability of TRN(Terrain Referenced Navigation). The accuracy of the altitude is one of the key parameters of TRN's accuracy. When the antenna of the IRA has wide beamwidth, its altitude accuracy is directly affected by the configuration of the earth's surface. Hence, the accuracy and reliability of TRN can also be affected and may cause ambiguity in positioning. We present analysis data for estimating the reliability of TRN by modeling several topographies and analyzing the performance of the IRA. The results of the analysis are verified by comparison with test data.

An Efficient Signal Processor for Interferometric Synthetic Aperture Radar Altimeter (레이더 간섭 고도계 처리 기법 개발)

  • Lee, Dong-Taek;Jung, Hyung-Sup;Yoon, Geun-Won
    • Proceedings of the Korean Association of Geographic Inforamtion Studies Conference
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    • 2010.06a
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    • pp.128-129
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    • 2010
  • 기존의 고도계는 레이더 특성에 의해 직하부의 높이 값을 정밀하게 관측할 수 없었다. 그러나 레이더 간섭 고도계는 SAR(Synthetic Aperture Radar) 영상의 칩 펄스(Chirp Pulse)를 이용한 고정밀 경사거리(Slant Range Distance)관측, 도플러 효과를 이용한 고정밀 경사각(Squint Angle)의 관측 및 레이더 간섭기법(SAR Interferometry)을 이용한 고정밀 관측각(Look Angle)의 관측을 가능하게 하였다. 이 연구의 목적은 레이더 간섭 고도계의 효율적인 신호처리 기법의 개발에 있다.

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Design and Implementation of FMCW Radar Signal Processor for Drone Altitude Measurement (드론 고도 측정용 FMCW 레이다 신호처리 프로세서 설계 및 구현)

  • Lim, Euibeen;Jin, Sora;Jung, Yongchul;Jung, Yunho
    • Journal of Advanced Navigation Technology
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    • v.21 no.6
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    • pp.554-560
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    • 2017
  • Accurate altimetry is required for the reliable flight control of drones or unmanned air vehicles (UAVs), and the radar altimeter is commonly used owing to its accuracy for the ground level. Due to the limitation for size, weight and power consumption, the frequency modulated continuous wave (FMCW) radar is appropriate for drone because it has lower complexity than that of pulse Doppler (PD) radar. Especially, fast-ramp FMCW radar, which transmits linear FM signal during very short period, is generally utilized, because it is robust for the ego-motion of drone. Therefore, we present the design and implementation results of the radar signal processor (RSP) for fast-ramp FMCW radar system. The proposed RSP was designed with Verilog-HDL and implemented with Altera Cyclone-IV FPGA device. Implementation results show that the proposed RSP includes 27,523 logic elements, 15,798 registers and memory of 138Kbits and can measure the altimeter at the rate of 100Hz with the operating frequency of 50MHz.