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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