Global Positioning System Reference
In-Depth Information
completing the square for
r
0
+
h
and taking the square root as
=
(r
0
+
h)
1
−
1
/
2
2
hr
0
(
1
−
cos
D
0
)
(r
0
+
r
=
[
(r
0
+
h)
2
−
2
r
0
h(
1
−
cos
D
0
)
]
1
/
2
h)
2
(
2
.
29
)
Since angle
D
0
is very small, it can be approximated as
D
0
2
1
−
cos
D
0
≈
(
2
.
30
)
where
D
0
is the angle expressed in radians. The
r
value can be written as
h)
1
−
h)
2
1
/
2
2
hr
0
D
0
/
2
(r
0
+
hr
0
D
0
2
(r
0
+
r
≈
(r
0
+
=
r
0
+
h
−
(
2
.
31
)
h)
At latitude of 45 degrees
D
0
(
≈
1/297 radian) becomes maximum. If
D
0
is
neglected, the result is
r
0
hD
0
2
(r
0
+
r
≈
r
0
+
h
−
h)
≈
r
0
+
h
(
2
.
32
)
Using this result, if
h
r
e
=
6368 km (the average radius of
the earth), the error term calculated is less than 0.6 m. Thus
=
100 km, and
r
0
=
h
=
r
−
r
0
(
2
.
33
)
is a good approximation. However, in this equation the value of
r
0
must be
evaluated, as discussed in Section 2.12.
2.12 CALCULATION OF GEODETIC LATITUDE
(
5-7
)
Referring to Figure 2.7, the relation between angles
L
and
L
c
can be found from
the triangle
OPC
. From the simple geometry it can be seen that
L
=
L
c
+
D
(
2
.
34
)
If the angle
D
can be found, the relation between
L
and
L
c
can be obtained.
To find this angle, let us find the distance
OC
first. Combining Equations (2.24)
and (2.27), the following result is obtained:
AE
tan
L
=
b
e
sin
β
tan
L
OC
=
OE
−
CE
=
a
e
cos
β
−
a
e
cos
β
−
e
e
)
]
a
e
e
e
cos
β
e
e
OE
=
a
e
cos
β
[1
−
(
1
−
=
=
(2.35)
where
β
is not shown in this figure but is shown in Figure 2.6.
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