2017
DOI: 10.3390/atmos8010014
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Evaluation of Surface Clutter for Future Geostationary Spaceborne Weather Radar

Abstract: Surface clutter interference will be one of the important problems for the future of geostationary spaceborne weather radar (GSWR). The aim of this work is to provide some numerical analyses on surface clutter interference and part of the performance evaluation for the future implementation of GSWR. The received powers of rain echoes, land and sea surfaces from a radar scattering volume are calculated numerically based on the derived radar equations, assuming a uniform rain layer and appropriate land and sea s… Show more

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Cited by 7 publications
(13 citation statements)
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“…The simulated results are consistent with Takahashi (2017) and Li et al (2017), suggesting that both…”
Section: Homogeneous Casesupporting
confidence: 73%
See 2 more Smart Citations
“…The simulated results are consistent with Takahashi (2017) and Li et al (2017), suggesting that both…”
Section: Homogeneous Casesupporting
confidence: 73%
“…However, the impact of the surface clutter and the oblique measurement would depend on the shape and position of the precipitation system. This study extends Li et al (2017) for a realistic case. By considering the importance to societal and scientific benefit, we chose a typhoon as a test case in this study.…”
Section: Introductionsupporting
confidence: 54%
See 1 more Smart Citation
“…Therefore, the antenna gain corresponding to the precipitation particles is different in different positions in a GSDWR beam element, so that the echo power is also different and must, therefore, be antenna weighted [25]. The weighting function expression is shown in Equation (15).…”
Section: Analysis Of the Simulation Resultsmentioning
confidence: 99%
“…Although the Geostationary Spaceborne Doppler Weather Radar (GSDWR) is still a conceptual radar [1,13,14], it has been studied in the United States and China and some of the related parameters of the radar system are shown in Table 1. The GSDWR is designed to work in geostationary orbit at an altitude of 36,000 km, with a maximum scan angle of 4 • , and a spiral scanned antenna beam [15]. The scan model is shown in Figure 1a.…”
Section: Gsdwr Introductionmentioning
confidence: 99%