2001
DOI: 10.1016/s0074-6142(01)80146-7
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Chapter 1 Satellite Altimetry

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Cited by 348 publications
(245 citation statements)
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“…The TOPEX, JASON1/JASON2/JASON3 missions all operate simultaneously at 13.575 GHz (Ku band) and 5.3 GHz (C band), flying at an identical orbit altitude (approximately 1336 km) with an inclination angle of 66 • and a period of 112 min [15,31,32]. By measuring the range on two different frequencies, the T/J altimeter can provide a direct vTEC VTEC T/J over the oceans (worst case of GNSS-derived vTEC) up to the T/J orbit altitude [17,22,33,34]. If Ku band ionospheric range correction is calculated as presented by Brunini et al [22], then the vTEC can be expressed as follows:…”
Section: Gnss-derived Vtec Data and Jason Vtec Datamentioning
confidence: 99%
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“…The TOPEX, JASON1/JASON2/JASON3 missions all operate simultaneously at 13.575 GHz (Ku band) and 5.3 GHz (C band), flying at an identical orbit altitude (approximately 1336 km) with an inclination angle of 66 • and a period of 112 min [15,31,32]. By measuring the range on two different frequencies, the T/J altimeter can provide a direct vTEC VTEC T/J over the oceans (worst case of GNSS-derived vTEC) up to the T/J orbit altitude [17,22,33,34]. If Ku band ionospheric range correction is calculated as presented by Brunini et al [22], then the vTEC can be expressed as follows:…”
Section: Gnss-derived Vtec Data and Jason Vtec Datamentioning
confidence: 99%
“…Jee et al [15] compared GPS vTEC and T/J vTEC for 1998-2009, and reported a positive relative TEC difference (i.e., GPS vTEC > T/J vTEC) in the PEC contribution to the ionosphere, which was largest in the early morning sector (up to 100%). However, many studies have found that T/J vTEC has a positive systematic bias of 2-5 TECu above real ionospheric TEC values when compared to other independent sources (i.e., T/J vTEC > GPS vTEC) [17][18][19][20][21][22][23]. This is paradoxical because GPS satellite altitude (~20,000 km) is higher than that of T/J satellites (~1336 km); thus, GPS vTEC should be larger than T/J vTEC due to it including the plasmasphere contribution above the T/J satellite orbital altitude.…”
Section: Introductionmentioning
confidence: 95%
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“…The Advanced Microwave Scanning Radiometer for the Earth Observing System (AMSR-E) sensor on-board the Aqua spacecraft had an effective footprint of 56 km [Chelton and Wentz, 2005], a swath width of approximately 1450 km [Martin, 2004] and provided approximately 89% coverage of the globe each day and 98% coverage every 2 days [Chelton and Wentz, 2005]. In contrast, the repeat orbit of satellite altimeters occurs at most once every 10 days and distances between altimeter tracks can be large-e.g., greater than 300 km for TOPEX/Poseidon tracks [Chelton et al, 2001]. The merger and optimal interpolation of altimeter data overcomes this limitation to some degree by combining measurements from multiple spacecraft but assumes certain temporal and spatial decorrelation scales during interpolation [Ducet et al, 2000;Le Traon et al, 2003].…”
Section: Microwave Sstmentioning
confidence: 99%
“…This estimation comprises the geoid (an equipotential of the earth gravity field to which a motionless ocean would exactly conform) and the ocean dynamic topography. The geoid has variations of up to 100 m and the ocean dynamic topography (the parameter of interest here) has variations of up to 1 m. For a comprehensive description of altimeter measurement principles, the reader is referred to Chelton et al (2001).…”
Section: Principle Of Satellite Altimetrymentioning
confidence: 99%