Geoscience Reference
In-Depth Information
These parameters must be calculated for all layers, and then it is possible to find the
total slant delay (
Δ
L d ) as follow
n
1
Δ
L d =
S i N i .
(116)
i
=
1
This equation can be divided into two terms for finding hydrostatic and non-
hydrostatic components of the delay separately. By inserting h i (along the zenith
direction) instead of S i (along the slant path) an equation for total zenith delay will
be derived. As mentioned before, the bending effect is a part of the total delay and
must be estimated separately. This parameter is zero for the zenith direction and
n 1
Δ
L b =
1 (
S i
cos
(
e i
e k )
S i ).
(117)
i
=
for a slant direction. Implementation of the above ray-tracing system can vary sub-
stantially, with different degrees of complexity and accuracy. Examples of ray-tracing
algorithms in atmospheric studies are given by Bean and Thayer ( 1959 ), Thayer
( 1967 ), Budden ( 1985 ), Davis ( 1986 ), Mendes ( 1999 ), Pany ( 2002 ), Böhmand Schuh
( 2003 ), Thessin ( 2005 ), Hulley ( 2007 ), Hobiger et al. ( 2008 ), Nievinski ( 2009 ),
Wijaya ( 2010 ), Gegout et al. ( 2011 ) and Nafisi et al. ( 2012a ). Several ray-tracing
algorithms were compared by Nafisi et al. ( 2012b ). Also it is possible to express the
Eikonal equation and the ray-tracing system in curvilinear non-orthogonal coordi-
nates systems. For details see Cerveny et al. ( 1988 ).
4.2 Mapping Functions and Gradients
In the analysis of space geodetic data the troposphere path delay
Δ
L
(
e
)
at the ele-
L z and an
vation angle e is usually represented as the product of the zenith delay
Δ
elevation-dependent mapping function mf
(
e
)
with
L z
Δ
L
(
e
) = Δ
·
mf
(
e
).
(118)
This concept is not only used to determine a priori slant delays for the observa-
tions, but the mapping function is also the partial derivative to estimate residual
zenith delays. Typically, the zenith delay is estimated with a temporal resolution of
20-60 min in VLBI and GPS analysis. In VLBI analysis—when there is only one
observation at a time at a station—this allows the zenith delays to be estimated in
a least-squares adjustment. In the analysis of space geodetic observations not only
the zenith delays are estimated, but also other parameters like the station clocks and
the stations heights (Fig. 8 ). The partial derivatives of the observed delays w.r.t. the
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