2017
DOI: 10.1002/2017jb014750
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Impact and Implementation of Higher‐Order Ionospheric Effects on Precise GNSS Applications

Abstract: High precision Global Navigation Satellite Systems (GNSS) positioning and time transfer require correcting signal delays, in particular higher‐order ionospheric (I2+) terms. We present a consolidated model to correct second‐ and third‐order terms, geometric bending and differential STEC bending effects in GNSS data. The model has been implemented in an online service correcting observations from submitted RINEX files for I2+ effects. We performed GNSS data processing with and without including I2+ corrections,… Show more

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Cited by 47 publications
(27 citation statements)
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“…where the subscript f = (1, 2, 3, · · ·) refers to a specific carrier frequency, superscript s refers to a specific satellite; ρ s r indicates the geometric distance between the satellite and receiver; dt r and dt s are the clock errors of receiver and satellite; dT is the slant tropospheric delay; dI s r,1 is the slant ionospheric delay on the first carrier frequency and a f = λ 2 f /λ 2 1 is the carrier frequency-dependent factor; D r, f and D s f are the receiver and satellite specific code hardware delays; λ f and N s r, f are the wavelength in meter and integer ambiguity in cycle; B r, f and B s f are the receiver-dependent and satellite-dependent uncalibrated phase delays; ε P f and ε Φ f are the pseudo-range and carrier phase measurement noise, respectively. Note that the higher-order ionospheric effects are neglected, as they have limited influence on the performance of ambiguity resolution [42].…”
Section: Uncombined Ppp Float Ambiguity Modelmentioning
confidence: 99%
“…where the subscript f = (1, 2, 3, · · ·) refers to a specific carrier frequency, superscript s refers to a specific satellite; ρ s r indicates the geometric distance between the satellite and receiver; dt r and dt s are the clock errors of receiver and satellite; dT is the slant tropospheric delay; dI s r,1 is the slant ionospheric delay on the first carrier frequency and a f = λ 2 f /λ 2 1 is the carrier frequency-dependent factor; D r, f and D s f are the receiver and satellite specific code hardware delays; λ f and N s r, f are the wavelength in meter and integer ambiguity in cycle; B r, f and B s f are the receiver-dependent and satellite-dependent uncalibrated phase delays; ε P f and ε Φ f are the pseudo-range and carrier phase measurement noise, respectively. Note that the higher-order ionospheric effects are neglected, as they have limited influence on the performance of ambiguity resolution [42].…”
Section: Uncombined Ppp Float Ambiguity Modelmentioning
confidence: 99%
“…The ionospheric delay could be expressed up to the third order, and the first order term (with a dependence on f −2 ) accounted for more than 99.9% of the total ionospheric delay. The higher-order ionospheric delay may exceed 10 mm (0.1 TECU [TEC Unit], 1 TECU = 1 × 10 16 electrons/m 2 ) [27], but the magnitude was very small in the global ionosphere mapping. The ionospheric delay could be expressed with a good approximation, without the higher-order ionospheric delay, as follows:…”
Section: Global Ionosphere Mapping Methodologymentioning
confidence: 99%
“…PPP can be an effective option for precise real-time positioning, but it requires more information than GNSS observations alone. Reliable satellite orbit and clock corrections [1][2][3][4][5], ionosphere [6] and troposphere model parameters [7], and antenna phase center offsets and variations must be provided in order to obtain precise results [8]. In PPP, orbit and clock errors are of major importance.…”
Section: Introductionmentioning
confidence: 99%