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k
l
j
k
l
% A (t
%
A (t
m
m
%
A (t
j
% A (t
Z WGS-84
k
%
B (t
l
%
B (t
j
%
B (t
m
%
B (t
B
b AB
A
Z B
Z A
Y WGS-84
Y B
X B
X A
X WGS-84
Y A
Fig. 5.3. Relative positioning
the relation
X B = X A + b AB
(5-10)
may be formulated, and the components of the baseline vector b AB
are
X B
X A
Y B − Y A
Z B
X AB
Y AB
Z AB
=
.
b AB =
(5-11)
Z A
The coordinates of the reference point must be given in the WGS 84 and are
usually approximated by a code pseudorange solution. Relative positioning
can be performed with code pseudoranges (cf. Eq. (5-3)) or with phase
pseudoranges (cf. Eq. (5-4)). Subsequently, only phase pseudoranges are
explicitly considered. We repeat (5-4),
λ Φ= + + λN,
(5-12)
where we have already explained the wavelength λ , the phase Φ, the distance
(which is the same as for the code pseudorange model), the speed of light
c , the receiver clock error δ , and the ambiguity N in Sect. 5.3.3.
Introducing f , the frequency of the corresponding satellite signal, and
taking into account the relation f = c/λ , we may divide (5-12) by λ obtain-
ing
Φ= 1
λ + + N.
(5-13)
This may be generalized to
Φ i ( t )= 1
λ i ( t )+ i ( t )+ N i
,
(5-14)
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