Global Positioning System Reference
In-Depth Information
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TABLE 4.2
Sequential Adjustment Models
Mixed Model
Observation Model
f
1
(
1
a
,
x
a
)
=
o
1
a
=
f
1
(
x
a
)
f
2
(
2
a
,
x
a
)
=
o
2
a
=
f
2
(
x
a
)
N
onlinear
model
P
1
O
OP
2
P
1
O
OP
2
P
=
P
=
B
1
v
1
+
A
1
x
+
w
1
=
o
v
1
=
A
1
x
+
Linear
1
model
B
2
v
2
+
A
2
x
+
w
2
=
o
v
2
=
A
2
x
+
2
B
1
P
−
1
B
1
B
2
P
−
1
B
2
P
−
1
1
P
−
1
2
M
1
=
M
2
=
M
1
=
M
2
=
Normal
equation
elements
1
2
A
1
M
−
1
A
2
M
−
1
A
1
P
1
A
1
A
2
P
2
A
2
N
1
=
A
1
N
2
=
A
2
N
1
=
N
2
=
[12
1
2
A
1
M
−
1
A
2
M
−
1
A
1
P
1
1
A
2
P
2
2
u
1
=
w
1
u
2
=
w
2
u
1
=
u
2
=
1
2
v
T
Pv
=
v
T
Pv
∗
+ ∆
v
T
Pv
v
T
Pv
=
v
T
Pv
∗
+ ∆
v
T
Pv
Lin
—
6.1
——
Nor
PgE
Minimum
v
T
Pv
∗
=−
u
1
N
−
1
u
1
+
w
1
M
−
1
v
T
Pv
∗
=−
u
1
N
−
1
T
1
P
1
1
u
1
+
w
1
1
1
1
v
T
Pv
(
A
2
x
∗
+
w
2
)
T
(
A
2
x
∗
+
2
)
T
∆
v
T
Pv
=
T
(
A
2
x
∗
+
w
2
)
∆
v
T
Pv
=
T
(
A
2
x
∗
+
2
)
x
∗
+ ∆
x
∗
+ ∆
x
=
x
x
=
x
N
−
1
1
N
−
1
1
x
∗
=−
x
∗
=−
u
1
u
1
E
stimated
=
M
2
+
A
2
−
1
=
P
−
1
2
A
2
−
1
p
arameters
A
2
N
−
1
A
2
N
−
1
T
T
+
1
1
A
2
T
A
2
x
∗
+
w
2
A
2
T
A
2
x
∗
+
2
N
−
1
1
N
−
1
1
∆
x
=−
∆
x
=−
[12
v
1
=
v
1
+ ∆
v
1
v
1
=
v
1
+ ∆
v
1
B
1
M
−
1
A
1
x
∗
+
w
1
Estimated
v
1
=−
P
−
1
v
1
=
A
1
x
∗
+
1
1
residuals
∆
v
1
=−
P
−
1
B
1
M
−
1
A
1
∆
x
∆
v
1
=
A
1
∆
x
1
1
E
stimated
va
riance of
v
T
Pv
v
T
Pv
2
0
2
0
σ
=
σ
=
r
1
+
r
2
−
u
n
1
+
n
2
−
u
unit weight
Estimated
Q
x
=
Q
x
∗
+ ∆
Q
Q
x
=
Q
x
∗
+ ∆
Q
p
arameter
Q
x
∗
=
N
−
1
1
Q
x
∗
=
N
−
1
1
cofactor
∆
Q
=−
N
−
1
1
A
2
TA
2
N
−
1
∆
Q
=−
N
−
1
1
A
2
TA
2
N
−
1
matrix
1
1
Because, in most cases the
P
1
matrix will be diagonal, no matrix inverse computation
is required. The size of the matrix
T
equals the number of observations in the second
group. Thus, if one observation is added at a time, only a 1
1 matrix must be inverted.
The residuals can be computed directly from the mathematical model as desired.
A third case pertains to the role of the weight matrix of the parameters. The weight
matrix expresses the quality of the information known about the observed parameters.
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