1 ee 543 theory and principles of remote sensing derivation of the transport equation

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1 EE 543 Theory and Principles of Remote Sensing Derivation of the Transport Equation

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Page 1: 1 EE 543 Theory and Principles of Remote Sensing Derivation of the Transport Equation

1

EE 543Theory and Principles of

Remote Sensing

Derivation of the Transport Equation

Page 2: 1 EE 543 Theory and Principles of Remote Sensing Derivation of the Transport Equation

O. Kilic EE 543

2

Theory of Radiative Transfer

We will be considering techniques to derive expressions for the apparent temperature, TAP of different scenes as shown below.

Atmosphere

Terrain

TA

TUP

TA

Terrain could be smooth, irregular, slab (such as layer of snow) over a surface.

STEP 1: Derive equation of radiative transferSTEP 2: Apply to different scenes

Page 3: 1 EE 543 Theory and Principles of Remote Sensing Derivation of the Transport Equation

O. Kilic EE 543

3

Radiation and Matter

• Interaction between radiation and matter is described by two processes:– Extinction– Emission

• Usually we have both phenomenon simultaneously.

• Extinction: radiation in a medium is reduced in intensity (due to scattering and absorption)

• Emission: medium adds energy of its own (through scattering and self emission)

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O. Kilic EE 543

4

Mediums of Interest

• The mediums of interest will typically consist of multiple types of single scatterers (rain, vegetation, atmosphere,etc.)

• First we will consider a single particle and examine its scattering and absorption characteristics.

• Then we will derive the transport equation for a collection of particles in a given volume.

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5

Apparent temperature distribution

Apparent Temperature (Overall Scene Effects)

antennaFn()

TA

Atmosphere

TAP()

TDN

TSC

TUP

TB

TB: Terrain emission

TDN: Atmospheric downward emissionTUP: Atmospheric upward emission

TSC: Scattered radiation

Terrain

SUMMARY

Page 6: 1 EE 543 Theory and Principles of Remote Sensing Derivation of the Transport Equation

Brightness

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6

• In radiometry, both point and extended source of incoherent radiation (e.g. sky, terrain) are of interest.

• Brightness is defined as the radiated power per solid angle per unit area, as follows:

• The unit for brightness is Wsr-1m-2

t

t

UB

A

Power per solid angle (W/Sr)

Function of ,

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O. Kilic EE 543

7

Apparent Temperature

• TAP() is the blackbody equivalent radiometric temperature of the scene.

2

2, ,i AP

kB T f

Incident brightnessConsists of several terms

SUMMARY

Similar in form to Planck’s blackbody radiation.

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8

Antenna Temperature (Overall Antenna Effects)

4

4

4

, ,

,

, ,

AP n

A

n

A A AP n

T F dT

F d

T T F d

We derived

Averaged temperature over the solid angle of receive antenna

Fn()

A

SUMMARY

TAP

TA

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9

Antenna Efficiency

• Radiation Efficiency

• Beam Efficiency: – Contributions due to sidelobes are undesired.– Ideally one would design a radiometer antenna

with a narrow pencil beam and no sidelobes.

' (1 )A a A a oT T T

SUMMARY

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10

Main Beam and Sidelobe Effects

4

4

1, ,

1, ,

1, ,

m

m

A AP n

r

AP n

r

AP n

r

A ML SL

T T F d

T F d

T F d

T T T

SUMMARY

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11

Main Beam Efficiency

4

( , )

( , )M

n

M

n

F d

F d

Ratio of power contained within the main beam to total power.

SUMMARY

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12

Effective Main Beam Apparent Temperature,

• Antenna temperature if the antenna pattern consisted of only the main beam.

, ,

,M

M

AP n

ML

n

ML ML ML

T F dT

F d

T T

MLT

SUMMARY

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13

Antenna Stray Factor

4

4

1

( , )

( , )S M

S M

n

n

F d

F d

SUMMARY

Ratio of power contained within the sidelobes to total power.

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14

Effective Sidelobe Antenna Temperature

, ,

,

(1 )

S

S

AP n

SL

n

SL SL SL ML SL

T F d

TF d

T T T

• Antenna temperature if the antenna pattern consisted of only the sidelobes.

SUMMARY

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Antenna Temperature and Beam Efficiency

(1 )A ML SL

ML ML ML SL

T T T

T T

SUMMARY

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16

Overall Antenna Efficiency and Antenna Temperature

' (1 )

(1 ) (1 )

A a A a o

a ML ML ML SL a o

T T T

T T T

Combine beam efficiency and radiation efficiency:

SUMMARY

Desired value

Measured value

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17

Linear relation1 1 1M a

ML A SL o

a M M a M

T T T T

MLT

AT

Bias = B1 +B2

-( B1 +B2)

Slope

Depends on sidelobe levels, antenna efficiency and temperature Depends on

antenna efficiency

SUMMARY

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Summary

The accuracy of radiometric measurements is highly dependent on the radiation efficiency, and main beam efficiency, of the antenna.M

a

SUMMARY

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19

Theory of Radiative Transfer

We will be considering techniques to derive expressions for the apparent temperature, TAP of different scenes as shown below.

Atmosphere

Terrain

TA

TUP

TA

Terrain could be smooth, irregular, slab (such as layer of snow) over a surface.

STEP 1: Derive equation of radiative transferSTEP 2: Apply to different scenes

SUMMARY

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20

Radiation and Matter

• Interaction between radiation and matter is described by two processes:– Extinction– Emission

• Usually we have both phenomenon simultaneously.

• Extinction: radiation in a medium is reduced in intensity (due to scattering and absorption)

• Emission: medium adds energy of its own (through scattering and self emission)

SUMMARY

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Terminology for Radiation/Scattering from a Particle

• Scattering Amplitude

• Differential Scattering Cross Section

• Scattering Cross Section

• Absorption Cross Section

• Total Cross Section

• Albedo

• Phase Function

SUMMARY

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Scattering Amplitudes and Cross Sections

• Brightness directly relates to power, and satisfies the transport equation.

• We will examine the effects of presence of scattering particles on brightness.

O

s

r

B(r,s) is a function of position and direction

Function of 5 parameters:r: x, y, zs:

SUMMARY

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Scattering AmplitudeConsider an arbitrary scatterer:

Imaginary, smallest sphere

D

i

Ei

o

Es

R

2

ˆˆ( , ) ; ,ikR

s o o i

e DE e f o i e E R

R

The scatterer redistributes the incident electric field in space:

SUMMARY

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Scattering Amplitude(2)

2

ˆˆ( , ) ; ,ikR

s o o i

e DE e f o i e E R

R

o: s, s

i: i, i

f(o,i) is a vector and it depends on four angles.

SUMMARY

Unit vectors along the incident and scattered directions

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Scattering Cross Section Definitions: Power Relations

• Differential Scattering Cross-section

• Scattering Cross-section

• Absorption Cross-section

• Total Cross-section

SUMMARY

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Differential Scattering Cross Section

2 2

ˆ ˆˆ ˆ, lim ,sd R

i

R So i f o i

S

o

i

RSi

SUMMARY

(m2/St)

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Scattering Cross-section

4

ˆ ˆˆ,ss d s

i

Pi o i d

S

SUMMARY

(m2)

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Absorption Cross-section

2

ˆ a Va

i i

E dvP

iS S

SUMMARY

(m2)

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Total Cross-section

t s a

tt s a

i

s

t

P P P

P

S

a

albedo

SUMMARY

(m2)

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Phase Function

ˆˆ ˆˆ ˆ, ,

ˆ ˆˆ ˆ, ,4

ˆ ˆˆ ˆ, ,

t

d

s

d

io i p o i

io i o i

p o i a o i

SUMMARY

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Phase Function (2)

4

4

1 ˆˆ,4

1 ˆˆ, 14

s

s

p o i d a

o i d

SUMMARY

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Derivation of the Radiative Transfer (Transport) Equation

v = a s

Consider a small cylindrical volume with identical scatterers inside.

The volume of the cylinder is given by:

Base area

0

a

s

Pout

Pin

s

s

length

rr + r

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Incident and Output Power

ˆIncident Brightness, ,

Incident Power:

ˆ ˆ , ,

Output Power:

ff

in f

out ff

B B r s

P B r s f a w B r s a w

P B B f a w

Change in brightness

(1)

(2)

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Conservation of Power

out in loss gainP P P P

Extinction:

off-scattering + absorption

self emission + scattering

(3)

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Extinction in the Cylindrical Volume Due to Scattering Phenomenon

N: # particles in volume V

: scattered power per particle

ˆ ˆ

s s

s

ins s i s

P N p

p

Pp i S i

a

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Scattering CoefficientLet denote the particle density in the volume.

s

Then

scattering coeffDefine icient " "

ins s s in

s

N NV a s

N a s

PP a s s P

a

N

ps

Unit: #/m

(4)

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Loss Due to Scattering

ˆ,

s s in

s s f

P s P

P sB r s f a w

(5)

Using (1) in (5)

(6)

s s

where

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Extinction in the Cylindrical Volume Due to Absorption Phenomenon

;

N: # particles in volume V

: absorbed power per particle

ˆ ˆ

ˆ

a a

a

ina a i a

ina a a in

P N p N a s

p

Pp i S i

aP

P a s i s Pa

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Absorption Coefficient

ˆ,a

a

f

a

aP sB r s f a w

Define “absorption coefficient: Unit: #/m

(7)

(8)

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Total Power Loss

ˆ,

ˆ,

loss s a

s a f

los

t s

s t f

a

P P P

B r s s a f w

P B r s s a f w

Define “total coefficient” or “extinction coefficient”

Total power loss is given by:

(9)

(10)

ˆ,s s fP sB r s f a w

ˆ,a a fP sB r s f a w

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Loss in Power - Summary

ˆ,loss t f

t a s

s s

a a

P B r s s a f w

Particle density in v

Incident Brightness

Due to scattering and absorption.

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Gain in the Cylindrical Volume Due to Scattering Phenomenon

s0

a

s

Pout

Pin

s

An increase in power is experienced when the particles scatter energy along s direction when they are illuminated from other directions; i.e. ˆ ˆ's s

ˆ 's

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Scattering of Incident Radiation Along s’ Towards s

2

Incident power density:

ˆ ˆ ' , ' '

Scattered power density per particle:

ˆ ˆ, 'ˆ ˆ '

Collective increase in power:

ˆ ˆ ˆ '

i f

d

r i

scatgain r r r r

r

S s B r s f w

s sS s S s

R

P s NS s A a s S s A

a s A

2

ˆ ˆ, 'ˆ, ' 'd

f

s sB r s f w

R

(11)

(12)

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Collective Increase in Power (2)

scatgain 2

scat scatgain gain

4

ˆ ˆ ˆ ˆ P ' , ' , ' '

ˆ ˆ ˆ , ' , ' '

Collective increase in power, from

possible incidence angles:

ˆ P P '

ˆ = ,

all

rd f

d f

d

As a s s s B r s f w

Ra s w s s B r s f w

s

s

4

ˆ ˆ' , ' 'fs B r s dw a s w f

(13)

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Collective Increase in Power

scatgain

4

scatgain

4

Using:

ˆ ˆ, 'ˆ ˆ ˆ ˆ , ' , ' and

4

ˆ ˆ ˆP , ' , ' '4

ˆ ˆ ˆ ˆor equivalently from , ' , '

ˆ ˆ ˆP , ' , ' '4

t

d

t t

tf

tf

s ss s p s s

p s s B r s dw a s w f

a s s p s s

a s s B r s dw a s w f

(14a)

(14b)

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Gain in the Cylindrical Volume Due to Self Emission

ˆ,emissiongainP r s s a f w

Define emission source function as power emitted per

(Volume Steradian Hertz) as ˆ,r s

(15)

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Total Increase in Power

4

ˆ ˆ ˆ, ' , ' '4

ˆ ,

scat emissiongain gain gain

tgain f

P P P

P p s s B r s dw a s w f

r s s a f w

(16)

Self emission

scattering

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Power Conservationout in loss gainP P P P From (3) i.e.

Using (1), (2), (10) and (16)

4

4

ˆ ˆ, ,

ˆ ˆ ˆ , ' , ' '4

ˆ ˆ + , ,

Divide by , take lim 0

ˆ,ˆ ˆ ˆ ˆ ˆ, , ' , ' ' ,

4

f t f

tf

ff

f tt ff

B r s f a w B r s a w f s

p s s B r s dw a w f s

r s a w f s B r s B a w f

s s

dB r sB r s p s s B r s dw r s

ds(17)

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Scalar Transport Equation

4

ˆ,ˆ,

ˆ ˆ ˆ, ' , ' '4

ˆ,

f

t f

tf

dB r sB r s

ds

p s s B r s dw

r s

Loss due to scattering and absorption

Gain due to scattering of other incident energy along s direction

Gain due to self emission

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Remarks on Emission Source Function

ˆ, : Power emitted/(Vol. St. Hz)

Under thermodynamic eq

thermal emission = absorption

uilibrium,

ˆ, ( )a f

r s

r s B T

a; absorption coefficient

#/m

Brightness of each particle inside the mediumPower/(St. Area. Hz)

Physical temperature

Directly proportional to absorption

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Self Emission Function

ˆ, ( ) ( )

(1 ) ( );

a f a f

st f

t

r s B T B T

a B T a

(18)

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Scalar Transport Equation – Based on Extinction Coefficient Only

4

ˆ,ˆ ˆ ˆ ˆ, , ' , ' '

4

(1 ) ( )

f tt f f

t f

dB r sB r s p s s B r s dw

ds

a B T

(19)

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Optical Distance

1

1,o

s

o ts

t

s s ds

d ds

0

s

s0

s1

ds

Dimensionless#

Loss factor per length

#t m

(20)

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Transport Equation as a Function of Optical Distance

t r

ˆ ˆ, ,ffB r s B s

Divide the transport equation in (19) by and express as a

function of ; i.e.

4

ˆ, 1ˆ ˆ ˆ ˆ, , ' , ' '

4

(1 ) ( )

f

f f

f

dB sB s p s s B s dw

d

a B T(21)

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Transport Equation as a Function of Optical Distance and Albedo

4

ˆ,ˆ,

ˆ ˆ ˆ, ' , ' '4

1 ( )

f

f

f

dB sB s

da

s s B s dw

a B T

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Transport Equation as a Function of Optical Distance

4

4

ˆ ˆMultiply by f, and let , ,

ˆ,ˆ ˆ, ,

1ˆ ˆ ˆ ˆ, , ' , ' ' 1 ( )

4

or

ˆ ˆ ˆ ˆ, , ' , ' ' 1 ( )4

Define

ˆ ˆ, ,

f

s a

B s B s f

dB sB s J s

d

J s p s s B s dw a B T

aJ s s s B s dw a B T

J s J s J T

Js Ja

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Solution to Transport Equation (1)

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Solution to Transport Equation (2)

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Solution to Transport Equation (3)

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Transport Equation Scaled to Temperature (1)

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Transport Equation Scaled to Temperature (2)

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Transport Equation Scaled to Temperature (3)

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Solution to Transport Equation (Temperature Form)

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Solution to Transport Equation

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'

0

ˆ ˆ ˆ, 0, ', 'AP AP TT s T s e J s e d

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Low Albedo Case, a<<1

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Solution for Low Albedo

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Upwelling Radiation (Observe the Medium from Above)

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Low Albedo Case, a <<1

cos

sec

sec

z s

s z

ds dz

sec

sec

t a a

a

d ds ds dz

d

dz

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Upwelling Radiation

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Upwelling Radiation

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Solution: Upwelling Radiation

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0

'

sec ' '

sec '' ''

0

, 0,

( ') sec ' '

z

a

z

a

z

z dz

AP AP

z z dz

a

T z T e

T z e z dz

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Example

Consider a downward looking, nadir pointing radiometer observing the ocean surface from an airborne platform above a 2 km thick cloud with water content of 1.5 g/m3. The absorption coefficient of the cloud is approximately given by:

where f is in GHz and mv is the water content in g/m3. Assuming that the ocean has an apparent temperature, TAP(0,0) of 150 K, calculate the apparent temperature observed by the radiometer at f = 1 GHz. The cloud may be assumed to have a physical temperature of 275K.

4 1.952.4 10a vf m

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Solution

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Solution

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Solution

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0

'

sec ''

0

0

,0 0,0

sec '

where

' 275

(0,0) 150

H

a

z

AP AP UP

H dz

UP o a a

AP

T H T e T

T T e dz

T z T

T

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Solution

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Solution

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Downwelling Radiation from a Layer (Observe the Medium from Below)

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cos

sec

seca a

H z s

ds

dzd ds dz

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Downwelling Radiation

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0

0

, ' sec '

, , sec '

s z

a a

s z H

z

a

H

r r ds dz

z H z H z dz

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Downwelling Radiation

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Downwelling Radiation

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'

'

sec '

sec ''

sec '

sec ''

, ,

' sec '

,

' sec '

z

a

H

z

a

z

H

a

z

z

a

z

dz

AP AP

z dz

a

H

dz

AP

H dz

a

z

T z T H e

T z e dz

T H e

T z e dz

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Summary

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'

' sec '

'' sec ''

, ,

' sec '

H

a

z

z

a

z

z dz

AP AP DN

H z dz

DN a

z

T z T H e T

T T z e dz

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Atmospheric Radiation

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84

Example

Atmospheric water vapor absorption coefficient at 22 GHz is

where v=moe-0.5z is the water vapor density (g/m3), and T=To-6.5z is temperature (K) and z is the altitute (km). Assuming that the most of the atmospheric absorption will be for the lowermost 10 km, calculate the downwelling and upwelling radiation temperatures for nadir direction. Let To = 300K and o = 7.5 g/m3

2

3 3006 10 Np/kma v T

Page 85: 1 EE 543 Theory and Principles of Remote Sensing Derivation of the Transport Equation

Solution

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Page 86: 1 EE 543 Theory and Principles of Remote Sensing Derivation of the Transport Equation

Solution

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Page 87: 1 EE 543 Theory and Principles of Remote Sensing Derivation of the Transport Equation

Solution

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Summary: Upwelling and Downwelling Radiation

',

0

, '

, sec ( ') ' '

, sec ( ') ' '

, sec ' '

zz z

UP a

Hz z

DN az

b

aa

T z T z e z dz

T z T z e z dz

a b z dz

Low Albedo Case

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Upwelling Radiation (Low Albedo)

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SPECIAL CASES:Constant Medium Temperature, T(z) = To

Uniform Particle Distribution, a(z) = ao

0 0

0'

0 0

0 0 0

0 0

0

0

0

( ', )0

0 '

sec ''( ', )

0 0

0 0

sec ( ') sec sec '

0 0

0 0

sec

0

sec '; ', sec ''

sec ' sec '

sec ' sec '

1sec

s

H

a

z

a a a

a

H Hz H

UP a a

z

H H dzz H

a a

H HH z H z

a a

H

aa

T T e dz z H dz

T e dz T e dz

T e dz T e e dz

T e

0

0

sec

sec

0

1ec

1

a

a

H

H

e

T e

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Downwelling Radiation (Low Albedo)

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SPECIAL CASES:Constant Medium Temperature, T(z) = To

Uniform Particle Distribution, a(z) = ao

0 0

'

00

0

0

0

0

0

0

0

(0, ')0

0 0

sec ''

0

0

sec '

0

0

sec

0

sec

0

sec '; 0, ' ' sec ''

sec '

sec '

1sec 1

sec

1

z

a

a

a

a

H Hz

DN a a

H dz

a

Hz

a

H

aa

H

T T e dz z z dz

T e dz

T e dz

T e

T e

Page 91: 1 EE 543 Theory and Principles of Remote Sensing Derivation of the Transport Equation

Special Cases: (Low Albedo)

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91

SPECIAL CASES:Constant Medium Temperature, T(z) = To

Uniform Particle Distribution, a(z) = ao

0sec

0 1 a H

DN UPT T T e

If layer H is several optical depths thick; aoH>>1

0DN UPT T T

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Apparent Temperature Inside the Medium

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SPECIAL CASES:Constant Medium Temperature, T(z) = To

Uniform Particle Distribution, a(z) = ao

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Application to Homogenous Half Space

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(eg. Soil, sea, etc.)

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Recall Conservation of Power

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12 12

12 12

2

12 12

1i r t i iP P P P P

R

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Homogenous Terrain Contributions

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95

There are two contributing factors to radiation observed from above:(1)Scattering of downward radiation from the atmosphere(2)Refraction of upward radiation from ground (terrain contribution)

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Terrain Contribution

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1 21 2

21 2

0 ,

1 0 ,

B AP

AP

T T

T

Upwelling radiation from a half space with uniform temperature

Recall that for an infinite layer of uniform temperature:

0DN UPT T T

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Terrain cont’ed

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Atmospheric Contribution

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1 12 1 1atm

sc DNT T

Downwelling atmospheric temperature

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Total Apparent Temperature for a Homogenous Half Space

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1 12 10 atmAP g DNT e T T

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Apparent Temperature at Altitude, H

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0,1 1

0,1 12 1

, 0, atm

atm

H atmAP AP UP

Hatmg DN

atmUP

T H T e T H

e T T e

T H

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References

• Microwave Remote Sensing, F. T. Ulaby, et.al. Addison-Wesley