Global Positioning System Reference
In-Depth Information
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which yields the following parameters and covariance matrix
N 1 ] T
z
=
[
ρ + ∆
I 1 ,P
N w
N 1
N 2
(7.29)
x Z T
Σ
=
Σ
Z
(7.30)
z
=
σ 1 , Φ =
U sing again the numerical values k
154 and
0 . 002 m, the standard devia-
tio ns and the correlation matrix become
σ ρ+∆ ,
σ 1 ,N = 0 . 99 m , 0 . 77 m , 0 . 28 cycL w , 9 . 22 cycL 1 (7.31)
σ I ,
σ w ,
1
0 . 9697
0 . 1230
0 . 9942
[24
1
0 . 1230
0 . 9904
C z =
(7.32)
1
0 . 0154
Lin
3.7
——
Nor
PgE
sym
1
The third parameter in (7.29) is the wide-lane ambiguity. We observed that there is
little correlation between the wide-lane and L1 ambiguities. Furthermore, the corre-
lations between the wide-lane ambiguity and both the topocentric distance and the
ionospheric parameter have been reduced dramatically. Considering the small stan-
dard deviation for the wide-lane ambiguity in (7.31) and its low correlations with
the other parameters, it should be possible to estimate the wide-lane ambiguity from
ep och solutions. The semiaxes of the ellipse of standard deviation for the ambiguities
ar e 9.22 and 0.28, respectively, and an orientation of 89.97° for the semimajor axis,
i.e ., the ellipse is elongated along the N 1 direction. The correlation matrix (7.32) still
sh ows high correlations between N 1 , the ionosphere, and the topocentric distance.
If we consider the square root of the determinant of the covariance matrix to be a
sin gle number that measures correlation, then (
[24
) 1 / 2
|
|
|
|
C z
/
C x
33 implies a major
de correlation of the epoch parameters.
The solution (7.29) is also obtained if we express the carrier phases (7.19) in cycles
an d then multiply with Z from the left. In fact, the following popular expressions can
be readily verified,
f 1 P 1 +
f 2 P 2
N w =
ϕ w
λ w +
f(
δ 1 ,P ,
δ 2 ,P ,
δ 1 ,
δ 2 )
(f 1 +
f 2 )
(7.33)
ϕ w
0 . 65 P 1
0 . 51 P 2 +···
ϕ w =
ϕ 1
ϕ 2
(7.34)
c
f w =
c
f 1
λ w =
f 2
0.86 m
(7.35)
 
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