Global Positioning System Reference
In-Depth Information
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With stated assumptions, Equation (6.38) becomes a standard differential equation
with all terms depending only on the intensity along the path of propagation. The
solution can be written as
s 0
I(f,s 0 )e −τ (s 0 )
B(f, T ) e −τ (s)
I(f, 0 )
=
+
α
ds
(6.41)
0
s
0 α
(s )ds
τ
(s)
=
(6.42)
Equation (6.41) is called the radiative transfer equation. I(f, 0 ) is the intensity at the
measurement location s
=
0, and I(f,s 0 ) is the intensity at some boundary location
s
=
s 0 . The symbol
τ
(s) denotes the optical depth or the opacity.
[20
kT , as is the case for microwaves and longer waves, the denominator
in (6.40) can be expanded in terms of hf / k T . After truncating the expansion, the
Planck function becomes the Rayleigh-Jeans approximation
If hf
Lin
5.5
——
No
PgE
2 f 2 kT
c 2
2 kT
λ
B(
λ
,T)
=
(6.43)
2
Th e symbol
denotes the wavelength. Expression (6.43) expresses a linear relation-
sh ip between Planck function and temperature T . For a given opacity (6.42) the in-
ten sity (6.41) is proportional to the temperature of the field of view of the radiometer
an tenna given (6.43).
The Rayleigh-Jeans brightness temperature T b (f ) is defined by
λ
[20
2
2 k I(f)
λ
T b (f )
(6.44)
T b (f ) is measured in degrees Kelvin; it is a simple function of the intensity of the
ra diation at the measurement location. If we declare the space beyond the boundary
s 0 as the background space, we can write the Rayleigh-Jeans background brightness
te mperature as
2
2 k I(f,s 0 )
λ
T b 0 (f )
(6.45)
=
Using definitions (6.44) and (6.45), the approximation (6.43), and T
T b , the
radiative transfer equation (6.41) becomes
s 0
T b 0 e −τ (s 0 )
e −τ (s) ds
T b =
+
T(s)
α
(6.46)
0
This is Chandrasekhar's equation of radiative transfer as used in microwave remote
sensing. For ground-based GPS applications, the sensor (radiometer) is on the ground
( s
=
0) and senses all the way to s
=∞
. T b 0 becomes the cosmic background
 
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