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f ; z m Þ ¼2 Z
H
z Þð R þ z Þ dz
ð R þ z Þ
t
;
q
;
2
2
ð R þ z m Þ
z m
where
cient, f is the sensing frequency, z is the height,
z m is the minimal distance of trace from Earth
ʳ
is the gas absorption coef
is radius, H is
the height of satellites orbits. A possibility of passive sensing of ClO, for instance,
is de
'
is surface, R is the Earth
'
ned by the expression for the limb brightness temperature:
z m Þ ¼2 Z
H
z Þð R þ z Þ
ð R þ z Þ
T ð z Þcð f
;
q
T j ð f
;
Q 1 ð z Þþ Q 2 ð z Þ
½
dz
;
2
2
ð R þ z m Þ
z m
where
0
1
Z
H
n
ð R þ nÞ
f
; nÞð R þ nÞ d
@
A;
Q 1 ð z Þ ¼0
:
5exp
q
2
2
ð R þ z m Þ
z
0
1
Z
H
n
ð R þ nÞ
f
; nÞ d
@
A
Q 2 ð z Þ ¼0
:
5exp
f
;
z m Þþ
q
2
2
ð R þ z m Þ
z
The radio-trauslusense method with using two satellites at frequencies of strong
gas absorption lines proves to be effective approach to the ozone layer characteristic
measuring (Strelkov 1995; Yakovlev 2001; Yakovlev et al. 2009). Enhancement of
this method is given by Yakovlev et al. (2009). Radio-eclipsing method of the Earth
sensing is proposed. Principal scheme of this method is characterized in Fig. 2.25 .
Fig. 2.25 Schematic diagram of global monitoring system based on the radio translusense method
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