2015 European Radar Conference (EuRAD) 2015
DOI: 10.1109/eurad.2015.7346279
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Theoretical and experimental investigations of a ground-based high-resolution SAR for buried object detection

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Cited by 6 publications
(8 citation statements)
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“…Assuming a beam width θ e = 40 • and a depression angle α= 45 • , the ground-range resolution is between 10 cm in the near and 5.5 cm in the far range. The usable swath width is approximately 2.5 m. Due to the low flight altitude the resolution in cross-range δ cr depends on the slant range R [6]:…”
Section: The Gpsar Sensor Modulementioning
confidence: 99%
“…Assuming a beam width θ e = 40 • and a depression angle α= 45 • , the ground-range resolution is between 10 cm in the near and 5.5 cm in the far range. The usable swath width is approximately 2.5 m. Due to the low flight altitude the resolution in cross-range δ cr depends on the slant range R [6]:…”
Section: The Gpsar Sensor Modulementioning
confidence: 99%
“…In recent years, the naval ships have been equipped with some particular facilities which consume very high short-time energy in an intermittent fashion, such as high power radars, electromagnetic guns, and solid-state lasers [1][2][3]. These facilities are referred to collectively as pulsed power loads (PPLs) [4], and the existing literature [5,6] presented that the PPLs are not only equipped on ships but also vehicles and other ground combat platforms. Whether on shipboard or land, the PPL is usually connected to the power supply, which has limited generation and small inertia.…”
Section: Introductionmentioning
confidence: 99%
“…In (6), ω represents the system frequency; d m represents the peak value of switching function at the fundamental frequency; respectively, V and φ are the RMS value and phase angle of the three-phase voltages. Further, from (1) to (5), if set…”
mentioning
confidence: 99%
“…Nevertheless, the implementation of these solutions is not straightforward in the context of UAVs. Ground-based GPR systems usually rely on large vehicles and trucks to carry large antenna arrangements (e.g., [30], [31], [32], [33], [34]). However, the integration of a GPR within a UAV is heavily constraint by the available space and weight in the platform, which directly impact the maximum flight time.…”
mentioning
confidence: 99%
“…In the case of [40] and [41], a single Tx is used, so the midpoint position changes when switching between Rx antennas. In contrast, a side-looking architecture is considered in [31], [32], and [33]. This system benefits from a significant separation between Txs and Rxs, which are also at different heights, to obtain 3-D images.…”
mentioning
confidence: 99%