Global Positioning System Reference
In-Depth Information
Fig. 2. The FKP positioning concept
The application of the positioning strategy is very simple. Four parameters, named E 0 , N 0 ,
E 1 , N 1 can be computed considering the estimated values of geometric and ionospheric
delays, using a given reference position (ϕ R , λ R ). After that, it is possible to calculate the
terms:
(
(
)
(
)
)
δ
r
=
6.37
N
ϕ ϕ
+
E
λ λ
cos
ϕ
0
0
R
0
R
R
(8)
(
)
(
)
(
)
δ
r
=
6.37
H N
ϕϕ
+
E
λλ ϕ
cos
I
1
R
1
R
R
where:
) 3
(
H
=+
1160.53
E π
/
(9)
where E is the satellite elevation (in radians). Finally, the two carrier-phase corrections (in
meters) are:
(
)
δ
r
=+
=+
δ
r
60 / 77
77 / 60
δ
r
f
1
0
I
(10)
(
)
δ
r
δ
r
δ
r
f
2
0
I
4.3 The MAC positioning
In 2001, Euler et al. (2001) had proposed a new approach to the use and transmission of
network corrections called Master Auxiliary Concept (MAC). The concept is the same as
above: a common level of network ambiguity fixing is estimated and the corrections are
transmitted to the rover separating dispersive and non-dispersive components.
In the MAC positioning, the coordinates and the biases of a single reference station (master
station) are broadcasted to the rover in addition to the single differences (both corrections
and coordinates) of the other stations in the network (auxiliary stations).
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