Global Positioning System Reference
In-Depth Information
1
2
φ
k =
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
Bv
+
Ax
+
w
=
o
(4.47)
1
2
φ
x =−
A T
k
=
o
(4.48)
Th e solution of (4.46) to (4.48) starts with the recognition that P is a square matrix
an d can be inverted. Thus, the expression for the residuals follows from (4.46):
P 1 B T k
v
=
(4.49)
Su bstituting (4.49) into (4.47), we obtain the solution for the Lagrange multiplier:
k
M 1 ( Ax
=−
+
w )
(4.50)
[10
with
Lin
* 1 ——
Lon
PgE
r M r = r B nn P nn B r
(4.51)
Finally, the estimate x follows from (4.48) and (4.50)
=− A T M 1 A 1 A T M 1 w
x
(4.52)
The estimates x and v are independent of the a priori variance of unit weight. The
first step is to compute the parameters x from (4.52), then the Lagrange multipliers k
from (4.50), followed by the residuals v (4.49). The adjusted parameters and adjusted
observations follow from (4.38) and (4.39).
The caret symbol in v , k , and x indicates that all three estimated values follow from
minimizing of v T Pv . However, as stated earlier, the caret is only used consistently for
the estimated parameters x in order to simplify the notation.
[10
4.4.3 Cofactor Matrices
Eq uation (4.44) shows that w is a random variable because it is a function of the
ob servation
b . With (4.37), the law of variance-covariance propagation (4.34), and
th e use of B in (4.42), the cofactor matrix Q w becomes
BP 1 B T
Q w
=
=
M
(4.53)
Fr om (4.53) and (4.52) it follows that
Q x = A T M 1 A 1
(4.54)
Combining (4.49) through (4.52) the expression for the residuals becomes
= P 1 B T M 1 A A T M 1 A 1 A T M 1
P 1 B T M 1 w
v
(4.55)
 
Search WWH ::




Custom Search