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Bernese GPS Software Version 5.0 - Bernese GNSS Software

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12. Ionosphere Modeling and Estimation<br />

12.2.2 Characterizing the Ionosphere<br />

The state of the ionosphere may be described by the electron density ne in units of electrons<br />

per cubic meter. The impact of the state of the ionosphere on the propagation of radio waves<br />

is characterized by the Total Electron Content E:<br />

E =<br />

S<br />

R<br />

ne(s)ds. (12.1)<br />

The integral gives the total number of free electrons included in a rotation cylinder with a<br />

cross-section area of one square meter, aligned along the signal path s between receiver R<br />

and satellite S. In geodetic applications, the TEC E is measured in so-called TEC Units<br />

(TECU), where one TECU corresponds to 10 16 electrons per square meter (10 16 /m 2 ). For<br />

comparisons, the vertical TEC Ev is formed as<br />

Ev = E cos z ′ , (12.2)<br />

where z ′ is the zenith distance of the signal path with respect to the vertical in a mean<br />

altitude of the ionospheric shell.<br />

The ionosphere is a dispersive medium in the radio-band – as opposed to the troposphere<br />

(see Chapter 11). This implies that ionospheric refraction depends on the frequency of the<br />

signal observed. Neglecting higher-order terms, we may write the ionospheric refraction<br />

coefficient for carrier phase measurements as<br />

nI = 1 − ane<br />

, (12.3)<br />

f2 where a is a constant, ne is the electron content along the signal propagation path, and f<br />

is the carrier frequency. The integration of Eqn. (12.3) along the entire propagation path s,<br />

taking into account Eqn. (12.1), yields the total effect of ionospheric refraction on phase<br />

measurements<br />

<br />

∆̺I =<br />

where E is the slant TEC.<br />

(nI − 1)ds = −<br />

s<br />

aE<br />

f2 with a = 4.03 · 10 17 m s −2 TECU −1 , (12.4)<br />

Formulae (12.3) and (12.4) indicate that the refractivity nI −1, and thus the refraction effect,<br />

is proportional to the inverse of the frequency squared. Consequently, if two frequencies are<br />

available, the ionospheric delay may be eliminated by forming the so-called ionosphere-free<br />

(L3) linear combination according to Eqns. (2.41) and (2.42).<br />

In the observation equation (Eqn. (2.34)), we defined a term I i k<br />

the ionospheric delay on L1:<br />

I i k<br />

= aE<br />

f 2 1<br />

Hence, the ionospheric delay may be written as<br />

that is synonymous with<br />

with f1 = 1.57542 · 10 9 s −1 . (12.5)<br />

∆̺I = ∓ f2 1<br />

f2 Ii k , (12.6)<br />

Page 256 AIUB

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