The GNSS integer ambiguities: estimation and validation
The GNSS integer ambiguities: estimation and validation
The GNSS integer ambiguities: estimation and validation
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2.2.3 Signal travel time<br />
In the preceding two sections the signal travel time τ s r in equations (2.7) <strong>and</strong> (2.12) has<br />
been assumed equal for code <strong>and</strong> phase measurements, as well as for measurements on<br />
different frequencies. In reality, this is not true since the signal travel time of the code<br />
actually is the group travel time. Moreover, the instrumental delays <strong>and</strong> atmospheric<br />
effects are different for the code <strong>and</strong> phase observations <strong>and</strong> for different frequencies.<br />
<strong>The</strong> difference between the travel times of different observation types <strong>and</strong> frequencies is,<br />
however, less than 10 −7 s corresponding to sub-millimeter satellite position differences<br />
(Teunissen <strong>and</strong> Kleusberg 1998). <strong>The</strong>refore, the travel times of all observation types are<br />
considered equal here.<br />
2.2.4 Instrumental delays <strong>and</strong> clock errors<br />
<strong>The</strong> receiver <strong>and</strong> satellite clock errors are independent of the observation type. On the<br />
other h<strong>and</strong>, the instrumental delays are different for code <strong>and</strong> phase measurements <strong>and</strong><br />
for different frequencies. Still, the instrumental delays <strong>and</strong> clock errors will be lumped<br />
together because it is not possible to separate the effects in a least-squares adjustment.<br />
Hence:<br />
dtr,j(t) = dtr(t) + dr,j(t)<br />
dt s ,j (t) = dts (t − τ s r ) − d s ,j (t − τ s r )<br />
δtr,j(t) = dtr(t) + δr,j(t)<br />
δt s ,j (t) = dts (t − τ s r ) − δ s ,j (t − τ s r )<br />
2.2.5 Atmospheric delays<br />
(2.13)<br />
<strong>GNSS</strong> signals have to travel through the earth’s atmosphere on their way from satellite<br />
to receiver. In the atmosphere neutral atoms <strong>and</strong> molecules, <strong>and</strong> charged particles<br />
are present that interact with the signals. This causes a propagation delay <strong>and</strong> signal<br />
absorption. <strong>The</strong> latter effect is not considered here. <strong>The</strong> propagation delay is caused<br />
by a deviation of the propagation speed from the velocity of light in vacuum, <strong>and</strong> an<br />
indirect delay due to signal bending. <strong>The</strong> delay is indicated with da <strong>and</strong> δa in equations<br />
(2.7) <strong>and</strong> (2.12) respectively.<br />
<strong>The</strong> atmosphere can be divided in different ”layers” with different characteristics. For<br />
<strong>GNSS</strong> especially the propagation characteristics are important, which means that the<br />
atmosphere needs to be divided into two ”layers”: the troposphere <strong>and</strong> the ionosphere.<br />
Tropospheric delays<br />
<strong>The</strong> troposphere is the lower part of the earth’s atmosphere <strong>and</strong> ranges from the surface<br />
to a height of approximately 9 km at the poles <strong>and</strong> to 16 km at the equator. In the<br />
troposphere neutral atoms <strong>and</strong> molecules are present, which cause a signal delay. <strong>The</strong><br />
troposphere is a non-dispersive medium at the <strong>GNSS</strong> frequencies, which means that<br />
10 <strong>GNSS</strong> observation model <strong>and</strong> quality control