Global Positioning System Reference
In-Depth Information
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
β
1
= β
(x
1
,y
1
,z
1
,x
2
,y
2
,z
2
)
(2.103)
s
=
s (x
1
,y
1
,z
1
,x
2
,y
2
,z
2
)
(2.104)
Th
e observables and parameters are
, respec-
tiv
ely. To find the elements of the design matrix, we require the total partial derivatives
wi
th respect to the parameters. The general form is
{α
1
,
β
1
,s
}
and
{
x
1
,y
1
,z
1
,x
2
,y
2
,z
2
}
dx
1
dy
1
dz
1
···
dx
2
dy
2
dz
2
d
α
1
g
11
g
12
g
13
g
14
g
15
g
16
d
x
1
···
d
x
2
=
β
1
ds
=
[
G
1
:
G
2
]
d
g
21
g
22
g
23
:
g
24
g
25
g
26
g
31
g
32
g
33
g
34
g
35
g
36
[47
(2.105)
Lin
—
0.3
——
No
*PgE
[
dx
i
dy
i
dz
i
]
T
. The partial derivatives are listed in Table 2.4. This
particular form of the partial derivatives follows from those of Wolf (1963), after
some additional algebraic manipulations.
with
d
x
i
=
TABLE 2.4
Partial Derivatives with Respect to Cartesian Coordinates
∂
α
1
∂x
1
=−
−
sin
ϕ
1
cos
λ
1
sin
α
1
+
sin
λ
1
cos
α
1
[47
g
11
=
g
14
=
(a)
s
cos
β
1
∂
α
1
∂y
1
=−
−
sin
ϕ
1
sin
λ
1
sin
α
1
−
cos
λ
1
cos
α
1
s
cos
β
1
g
12
=
g
15
=
(b)
∂
α
1
∂z
1
=−
cos
ϕ
1
sin
α
1
s
cos
β
1
g
13
=
g
16
=
(c)
∂
β
1
∂x
1
=−
g
24
=
−
s
cos
ϕ
1
cos
λ
1
+
sin
β
1
∆
x
s
2
cos
β
1
g
21
=
(d)
∂
β
1
∂y
1
=−
g
25
=
−
s
cos
ϕ
1
sin
λ
1
+
sin
β
1
∆
x
g
22
=
(e)
s
2
cos
β
1
∂
β
1
∂z
1
=−
g
26
=
−
s
sin
ϕ
1
+
sin
β
1
∆
z
g
23
=
(f)
s
2
cos
β
1
∂s
∂x
1
=−
−∆
x
g
31
=
g
34
=
(g)
s
∂s
∂y
1
=−
−∆
y
g
32
=
g
35
=
(h)
s
∂s
∂z
1
=−
g
36
=
−∆
z
g
33
=
(i)
s