2017
DOI: 10.1016/j.asr.2016.09.002
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Seasonal and solar cycle effects on TEC at 95°E in the ascending half (2009–2014) of the subdued solar cycle 24: Consistent underestimation by IRI 2012

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Cited by 11 publications
(5 citation statements)
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“…Therefore, the vertical TEC italicVTEC=()italicSTEC()bR+bs/S()E, where E is the elevation angle of the satellite in degrees, S ( E ) is the obliquity factor with zenith angle at the ionospheric piece point (IPP), and VTEC is the vertical TEC at the IPP. Other details of VTEC retrievals for DBRG are given in Kakoti et al (2017, 2018). In the present study, the hourly average VTEC is calculated as the average of VTEC (hereinafter TEC) obtained from all the passes received in each hour for respective GPS receiver stations with elevation cutoff 50°.…”
Section: Methodsmentioning
confidence: 99%
“…Therefore, the vertical TEC italicVTEC=()italicSTEC()bR+bs/S()E, where E is the elevation angle of the satellite in degrees, S ( E ) is the obliquity factor with zenith angle at the ionospheric piece point (IPP), and VTEC is the vertical TEC at the IPP. Other details of VTEC retrievals for DBRG are given in Kakoti et al (2017, 2018). In the present study, the hourly average VTEC is calculated as the average of VTEC (hereinafter TEC) obtained from all the passes received in each hour for respective GPS receiver stations with elevation cutoff 50°.…”
Section: Methodsmentioning
confidence: 99%
“…Almost equal levels of saturation effects were observed during the June solstice for MSA and HSA. Liu et al [58] and Kakoti et al [59] suggested that changes in solar EUV, thermospheric neutral wind composition and ion pressure were also important factors that may give rise to the saturation effect during different epochs of the solar cycle. Hence, the reason behind the generation of the saturation effect should be further investigated to understand its effects on satellite launch processes and satellite Radio communication devices.…”
Section: Discussionmentioning
confidence: 99%
“…From these figures, it is perceived that descending orbits present much higher FRA and higher dynamic ranges than ascending ones. In the afternoon local time, the surviving amount of VTEC generated by sunlight during the preceding hours is higher than in the morning local time [19] and because SMOS is in a 6 am-6 pm sun-synchronous orbit, the resulting FRA range is large. Consequently, in the first stage, the analysis was focused on descending orbits.…”
Section: Faraday Rotationmentioning
confidence: 96%
“…It is known that the VTEC and therefore the FRA vary with solar activity, which can be assessed using sunspot numbers [18], and in a geographical and temporal way [7,19]. SMOS data is here It is known that the VTEC and therefore the FRA vary with solar activity, which can be assessed using sunspot numbers [18], and in a geographical and temporal way [7,19]. SMOS data is here considered within the 24th sun cycle, which started on January 4th, 2008, with each cycle lasting about 11 years.…”
Section: Faraday Rotationmentioning
confidence: 99%
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