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Page 1: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23 UPR, Mayagüez Campus

Radiometer Systems

INEL 6669 microware remote sensing

S. X-Pol

Page 2: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

RxTx Rx

Radar

(active sensor)Radiometer

(passive sensor)

Microwave Sensors

Page 3: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23 UPR, Mayagüez Campus

Radiometers

Radiometers are very sensitive receivers that measure thermal electromagnetic emission (noise) from material media.

The design of the radiometer allows measurement of signals smaller than the noise introduced by the radiometer (system’s noise).

Page 4: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23 UPR, Mayagüez Campus

Topics of Discussion

Equivalent Noise TemperatureNoise Figure & Noise Temperature

Cascaded SystemNoise for AttenuatorSuper-heterodyne Receiver

System Noise Power at AntennaRadiometer Operation

Measurement Accuracy and PrecisionEffects of Rx Gain Variations

Page 5: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Topics of Discussion…

Dicke RadiometerBalancing Techniques

Reference -Channel ControlAntenna-Channel Noise-InjectionPulse Noise-InjectionGain-Modulation

Automatic-Gain Control (AGC) Noise-Adding radiometerPractical Considerations &Calibration

Techniques

Page 6: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Radiometer’s Task: Measure antenna temperature, TA’ which is proportional to TB, with sufficient radiometric resolution and accuracy

TA’ varies with time.

An estimate of TA’ is found from Vout and the radiometer

resolution T.

Rad

iom

eter

TA

TA’

Vout

TB

Page 7: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Noise voltage

The noise voltage is

the average=0 and the rms is

kTBRkThf

hfBR

e

hfBRV

JeansRayleighkThfn 4

/

4

1

4/

kTBRVV nrms 422

Page 8: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Noisy resistor connected to a matched loadis equivalent to… [ZL=(R+jX)*=R-jX]

kTBR

kTBR

R

VVIVP rmsrms

nn

4

4

22

Independent of f and R!,

Page 9: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Equivalent Output Noise Temperature for any noise source

BkTP Eno

TE is defined for any noise source when connected to a matched load. The total noise at the output is

ATIdeal Bandpass Filter

B, G=1

ZL

BkTP AA'

Receiverantenna

'AT

Page 10: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Noise Figure, F Measures degradation of noise through the device

is defined for To=290K (62.3oF!, this = winter in Puerto Rico.)

noso

nisi

oo

ii

PP

PP

NS

NSF

/

/

/

/

oE TFT )1(

Total output signal

Total output noise

Noise introduced by device

input signal

input thermal noise

Page 11: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Noise Figure, F

Noise figure is usually expressed in dB

Solving for output noise power

nonino

siso

PGPP

GPP

BGkT

P

BkT

PBGkT

GPP

PP

PP

PPF

o

no

o

noo

niso

nosi

noso

nisi

1

1

/

/

FFdB log10

niono FGPBFGkTP BGkTFP ono )1(

Page 12: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Equivalent input noise TE

Noise due to device is referred to the input of the device by definition:

So the effective input noise temp of the device is

Where, to avoid confusion, the definition of noise has been standardized by choosing To=290K (room temperature)

BGkTBGkTFP Eiono )1(

oEoE TTFTFT /1or )1(

Examples: 1dB NF is

and 3dB NF is What is TE for F=2dB?

170K

75K

288K

Page 13: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23 UPR, Mayagüez Campus

Cascade System

BTTkGG

PPGG

BG

TTTkGG

PGPGGPGGP

E

Ein

EE

EEnino

121

21

1

21121

2212121

1

21 G

TTT E

EE

1

21

11

G

FF

T

TF

o

E

Page 14: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

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Noise of a cascade system

12121

3

1

21 ...

1...

11

N

N

GGG

F

GG

F

G

FFF

12121

3

1

21 ...

...

N

ENEEEE GGG

T

GG

T

G

TTT

Page 15: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

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Noise for an Attenuator

BkTBkTLPLP

PBkTL

P

BkTP

P

PGL

EpnoE

nopno

pno

o

i

)1(

1

1/1

LTTLF

TLT

where

op

pE

/)1(1

)1(

Page 16: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Antenna, TL and Rx

1

21'

G

TTT E

EREC

dBLKTKT

Example

prec 5.,290,50

:

KT

yields

REC 5.91'

...

ReceiverReceiver

TTE2E2

Transmission

Line, TE1

Page 17: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

Superheterodyne Receivers Rx in which the RF amplifier is followed by a mixer that

multiplies the RF signal by a sine wave of frequency LO generated by a local oscillator (LO).  The product of two sine waves contains the sum and difference frequency components

The difference frequency is called the intermediate frequency (IF).  The advantages of superheterodyne receivers include doing most of the amplification at lower frequencies (since

IF<RF), which is usually easier, and precise control of the RF range covered via tuning only the local

oscillator so that back-end devices following the un-tuned IF amplifier, multichannel filter banks or digital spectrometers for example, can operate over fixed frequency ranges.

04/10/23

)t] cos[-)t]-cos[(t)t)sin(2sin( RFLORFLORFLO

Page 18: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

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RF amp G rf ,F rf ,T rf

Superheterodyne receiver

...MRF

IF

RF

MRFREC GG

T

G

TTT

MixerLM,FM,TM

IF amp G if ,F if ,T if

LO

Pni Pno

G=30dBF=2.3dB

G=23dBF=7.5dB

G=30dBF=3.2dB

Example:Trf=290(10.32-1)=638KTm=1,340KTif=203KTREC=?

KTREC 34.639...20010

203

10

1340638

33

Page 19: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

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Equivalent System noise power at antenna terminals

Taking into consideration the losses at the antenna and T.L. with a physical temperature of Tp:

ReceiverReceiver Transmission

Line

ARECsys PPP ''

BLTTLkBkTP

BTTkBkTP

TTT

RECpRECREC

plAlAA

plAlA

)1(''

and

)1(''

then,

)1(' Given

Page 20: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Equivalent System noise power at antenna terminals

Then the total noise for the system is:

ReceiverReceiver Transmission

Line

RECpplAlsys

RECpplAlsys

sysRECASYS

LTTLTTT

or

BLTTLTTkBkT

BkTPPP

)1()1(

)1()1(

''

For radiometer , Psys = Prec

For Radar, S/N= Pr/Psys

Page 21: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Summary

Antenna

Antenna + losses

Receiver

Receiver + T.L.

All of the aboveBkTP

P

P

P

P

sysSYS

REC

REC

A

A

'

'

Page 22: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

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Measurement Accuracy and Precision

Accuracy (“certeza”) – how well are the values of calibration noise temperature known in the calibration curve of output corresponding to TA

‘ . (absolute cal.)

Precision (“precisión”)– smallest change in TA

‘ that can be detected by the radiometer output.(sensitivity) T

Page 23: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23 UPR, Mayagüez Campus

Total Power Radiometer

Super-heterodyne receiver: uses a mixer, L.O. and IF to down-convert RF signal. Usually BRF>BIF

Page 24: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23 UPR, Mayagüez Campus

Detection- power spectra @:

deviation standard theis where

voltagespositivefor )(

envelope

withmean, zero with noiseGaussian

as drepresente is voltageIF the

noise thermalis spectraPower

'' where

''

2

2

22

eV

ee

SYSIF

RECASYS

SYS

RECASYS

eV

Vp

BGkTP

TTT

BkT

PPP

From Ulaby, Moore & Fung, 1986

Page 25: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

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Noise voltage after IF amplifier

deviation standard theis where

2

1R Assuming

2

is voltagesquare noise for the mean value theshown that becan It

22

22

eIF

e

VP

V

IFddedd

dd

edd

d

PCCVCV

μV/μW CC

VCV

V

22

2

2

is oltagedetector v of valueaverage The

7 e.g. constant,detector theis where

is detector, law-square theofoutput The

SYSdGkBTC

IF

Page 26: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Noise voltage after detector, Vd

V

σ

V

V

V

eV

Vp

dVVpdVVp

d

d

dd

dd

dd

V

V

d

d

eedd

d

d

1

or 1/ So,

is of variancethe

1

)(Then

)()(

Since

22

22

represents the average value or dc, and d represents the rms value of the ac component or the uncertainty of the measurement.

dV

IFx2

square-lawdetector

Ve Vd

Page 27: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Noise voltage after Integrator

Integrator (low pass filter) averages the signal over an interval of time .

Integration of a signal with bandwidth B during that time, reduces the variance by a factor N=Bwhere B is the IF bandwidth.

BV

σ

BV

σ

V

σ

out

out

IFd

d

out

out

1

or

1

filter pass-low theofoutput at the voltageThe

2

2

2

2

x2

integrator

Low-pass , gLF

VoutVdVe

Page 28: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

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Radiometric Resolution, T

The output voltage of the integrator is related to the average input power, Psys

VgV dLFout

x2

integrator

Low-pass , gLF

SYSS

SYSdLF

TG

GkBTCg

BT

T

V

σ

sys

sys

out

out

1

B

TT

B

TT RECAsys

sys

''

VoutVdVe

Page 29: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

Noise averaging

By averaging a large number N of independent noise samples, an ideal radiometer can determine the average noise power and detect a faint source that increases the antenna temperature by a tiny fraction of the total noise power.

http://www.cv.nrao.edu/course/astr534/Radiometers.htmlhttp://www.millitech.com/pdfs/Radiometer.pdf

04/10/23

Page 30: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

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Receiver Gain variations

Noise-caused uncertainty

Gain-fluctuations uncertainty

Total rms uncertainty

B

TT SYS

N

S

SSYSG G

GTT

22GN TTT

Example p.368T’Rec=600KT’A=300KB=100MHz=0.01sec

Find the radiometric resolution, T

01.

S

S

G

G

Page 31: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

Gain Variations and Dicke radiometer

As you can see gain variations in practical radiometers, fluctuations in atmospheric emission, and confusion by unresolved radio sources may significantly degrade the actual sensitivity compared with the sensitivity predicted by the ideal radiometer equation.

One way to minimize the effects of fluctuations in both receiver gain and atmospheric emission is to make a differential measurement by comparing signals from two adjacent feeds. The method of switching rapidly between beams or loads is called Dicke switching after Robert Dicke, its inventor. [Using a double throw switch.]

04/10/23

Page 32: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

2

222

222

'2/

'

2/

'' refA

S

SRECrefRECA

GrefNantN

TTG

G

B

TT

B

TT

TTTT

Page 33: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

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Dickie Radiometer

Noise-caused uncertainty

Gain-fluctuations uncertainty

Total rms uncertainty

B

TT SYS

N

S

SSYSG G

GTT

22GN TTT

QuizT’Rec=500KT’A=150KB=100MHz=1msec

Find the radiometric resolution, T

unknownG

G

S

S

2

222

222

''2''2

refAS

SRECrefRECA

GrefNantN

TTG

G

B

TTTT

TTTT

Page 34: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Dicke Radiometer

•Dicke Switch

•Synchronous Demodulator

Noise-Free

Pre-detection Section

Gain = G

Bandwidth = B

Switching rate, fs= 1/s

Page 35: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Dicke Radiometer

'''2

1RECREFRECASout TTTTGV

REFAS

SG TT

G

GT

'

The output voltage of the low pass filter in a Dicke radiometer looks at reference and antenna at equal periods of time with the minus sign for half the period it looks at the reference load (synchronous detector), so

The receiver noise temperature cancels out and the total uncertainty in T due to gain variations is

Page 36: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

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Dicke radiometer

The uncertainty in T due to noise when looking at the antenna or reference (half the integration time)

Unbalanced Dicke radiometer resolution

2

222

222

''2''2

refAS

SRECrefRECA

refNantNG

TTG

G

B

TTTT

TTTT

B

TTT RECref

refN

'2

B

TT

B

TTT RECARECA

antN

''2

2/

''

Give example: B=100MHz, =1s, T’rec= 700K, G/G=.01, Tref=300K for T’A=0K and 300K, for Total P radiometer and Dicke radiometer

Page 37: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

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Balanced Dicke

ideal

RECASYS

refAS

SRECrefRECA

refNantNG

TB

TT

B

TT

TTG

G

B

TTTT

TTTT

2''22

''2''2

222

222

A balanced Dicke radiometer is designed so that TA’= Tref at all times. In this case,

Page 38: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

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Balancing Techniques

Reference Channel ControlAntenna Noise InjectionPulse Noise InjectionGain ModulationAutomatic Gain Control

Page 39: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Reference Channel Control

oN

ref TLL

TT

11

VoutSynchronousDemodulator

Tref

Pre-detection

G, B, TREC’

Feedback

and

Control circuit

Switch driver andSquare-wave generator, fS

Integrator

LVariableAttenuatorat ambient

temperature

To

Vc

TN

Noise Source

TA’

oref

Nref

refA

TTL

TTL

TT

if

1 if

'

Force T’A= T ref

Page 40: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Reference Channel Control

TN and To have to cover the range of values that are expected to be measured, TA ’

If 50k<TA’< 300K

Use To= 300K and need cryogenic cooling to achieve TN =50K.

But L cannot be really unity, so need TN < 50K. To have this cold reference load, one can use cryogenic cooled loads (liquid nitrogen submerged passive

matched load) active “cold” sources (COLDFET); backward terminated LNA can

provide active cold source.

oAN TTT '

Page 41: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Cryogenic-cooled Noise Source

When a passive (doesn’t require power to work) noise source such as a matched load, is kept at a physical temperature Tp , it delivers an average noise power equal to kTpB

Liquid N2 boiling point = 77.36°K

Used on ground based radiometers, but not convenient for satellites and airborne systems.

Page 42: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Active “cold or hot” sources

http://www.maurymw.com/

http://sbir.gsfc.nasa.gov/SBIR/successes/ss/5-049text.html

Page 43: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Ideal radiometer

“Real” radiometer

Usually we wantT=1K,so we need B=100MHz and =10msec

B

TTT NA

B, G

radiometerTA

Pn=k B G TA

B, G

radiometer

TA =200K

Pn=k B G (TA + TN)

TN =800K

Page 44: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Active noise source: FET

The power delivered by a noise source is characterized using the ENR=excess noise ratio

where TN is the noise temperature of the source and To is its physical temperature.

ENRENR

T

T

kBT

TTkB

P

PPENR

dB

o

N

o

oN

o

on

log10

1)(

)(

Example for 9,460K: ENR= 15 dB

Page 45: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Antenna Noise Injection

cA

c

NA

orefA

FT

F

TT

TTT

11'

'"

"

VariableAttenuator

VoutSynchronousDemodulator

Tref

Coupler Pre-detection

G, B, Trec’

Feedback

and

Control circuit

Switch driver andSquare-wave generator, fS

Integrator

L Vc

TN

Noise Source

TA’TA”

L

T

LTT N

oN

11'

T’N

Force T”A= T ref = T o

Fc = Coupling factor of the directional coupler

*Measures vc

Page 46: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Antenna Noise Injection

Combining the equations and solving for L

from this equation, we see that To should be >TA’

If the control voltage is scaled so that Vc=1/L, then Vc will be proportional to the measured temperature,

'1 AoC

oN

TTF

TTL

'1Ao

oN

CC TT

TT

FV

'

AT

Page 47: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Example: Antenna Noise Injectio

K

B

TTT

L

KT

F

KTK

RECo

N

c

A

02.2'2

50-1.93between vary tohas

ENR) (22dB 000,50

100)(Coupler ldirectiona dB20

30050 '

'1 from

AoC

oN

TTF

TTL

Page 48: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Example: Antenna Noise Injection

If 50K< TA’< 300K, need to choose To>300K, say To=310K

If Fc=100(20dB) and Tn=50,000K

Find L variation needed:

'1 AoC

oN

TTF

TTL

KTforL

KTforL

A

A

3002.50

5093.1'

'

Page 49: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Antenna Noise Injection

For expected measured values between 50K and 300K, Tref is chosen to be To=310K, so

Since the noise temperature seen by the input switch is always To , the resolution is

B

TTT RECo '2

L

Page 50: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Pulse Noise Injection

poON

AoCR TT

TTFf

'

'1

cA

c

NA

orefA

FT

F

TT

TTT

11'

'"

"

LT

L

TT o

NN

11'

VoutSynchronousDemodulator

Tref

Coupler Pre-detection

G, B, Trec’

Feedback

and

Control circuit

Switch driver andSquare-wave generator, fS

Integrator

Pu

lse-

Atte

nu

atio

n

Dio

de

sw

itch

f r

TNNoise Source

TA’TA”

TN’

offo

off

Noff L

TL

TT

11'

*Measures fr

ono

on

Non L

TL

TT

11'

Page 51: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Pulse Noise Injection

for

0for

'

'

'

RpOFF

pON

N

tT

tT

T

R

p Pulse repetition frequency = fR = 1/R

Pulse width is constant = p

Square-wave modulator frequency fS< fR/2

Switch ON – minimum attenuation

Switch Off – Maximum attenuation

off

N

offoOFF L

T

LTT

11'

Example:For Lon = 2, Loff = 100 , To = 300K

and TN = 1000K,

We obtain Ton= 650K, Toff= 307K

Diode switch

TN

TN’

T’on

T’off

Page 52: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Pulse Noise Injection

Reference T is controlled by the frequency of a pulse

The repetition frequency is given by

''' )1( OFFRpRpONN TffTT

c

NA

coA F

TT

FTT

''" 1

1

poON

Aoc

pOFFON

ACOFFoCR TT

TTF

TT

TFTTFf

'

'

''

'' ))(1(1

For Toff = To, is proportional to T’A

Page 53: 6/6/2014UPR, Mayagüez Campus Radiometer Systems INEL 6669 microware remote sensing S. X-Pol

04/10/23

Example; Pulse Noise-Injection

With:

needed rangefrequency Find

300'60

50

5.1

20

315

10

sec20p

KTK

dBL

dBL

dBENR

KT

dBF

A

off

on

o

c

HzfKT

kHzfKT

KT

KT

KT

F

Answers

rA

rA

on

off

N

c

302,300'

5,60'

22615

315

815,31

10

:

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Gain-Modulation

Vout

SynchronousDemodulator

Pre-detection

G, B, Trec’

Control circuit

Switch driver andSquare-wave generator, fS

Integrator

v c

Tref

TA’

*Measures vc

Fixed attenuator

Lo

Variable attenuator

Lv

ocref

cA

vc

crefv

cAo

vout

LTT

TT

Lv

TTL

TTL

Lv

11

: thatso voltagecontrol theScale

11

:condition hemaintain t to vary 0, for

'Re

'

'Re

'

'Re

''Re

'

Drawback: slow variations of receiver noise temperature, yields error in reading.

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Automatic-Gain-Control AGC

Feedback is used to stabilize Receiver Gain Use sample-AGC not continuous-AGC since this would

eliminate all variations including those from signal, TA’.

Sample-AGC: Vout is monitored only during half-cycles of the Dicke switch period when it looks at the reference load.

Hach in 1968 extended this to a two-reference-temperature AGC radiometer, which provides continuous calibration. This was used in RadScat on board of Skylab satellite in 1973.

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Automatic Gain-Control (AGC)

Vagc

SynchronousDemodulator

2fs

Pre-detection

G, B, Trec’

Feedback

amplifier

Switch driver andSquare-wave generator, fS

Integrator

Gv

Reference

Switch

2fs

T2T1

gv

SynchronousDemodulator

fs

fs

Hach radiometer: insensitive to variations from G, and Trec’.

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Dicke Switch

Two types Semiconductor diode switch, PINFerrite circulator

Switching rate, fS , High enough so that GS remains constant over

one cycle.To satisfy sampling theorem, fS >2BLF (Same

as saying that Integration time is =1/2BLF)

http://envisat.esa.int/instruments/mwr/descr/charact.html

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Dicke Input Switch

Important properties to consider

Insertion loss Isolation Switching time Temperature stability

http://www.erac.wegalink.com/members/DaleHughes/MyEracSite.htm

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Radiometer Receiver Calibration

Most are linear systems

Hach-radiometer is connected to two known loads, one cold (usually liquid N2), one hot.

Solve for a and b. Cold load :satellites

use outer space ~2.7K

)(

)(

bTai

bTaicold

calcoldout

hotcal

hotout

rcAout fvbTai or or )( '

hotoutv

coldoutv

hotcalTcold

calT

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Imaging Considerations

Scanning configurationsElectronic (beam steering)

Phase-array (uses PIN diode or ferrite phase-shifters, are expensive, lossy)

Frequency controlled

Mechanical (antenna rotation or feed rotation)Cross-track scanningConical scanning (push-broom) has less

variation in the angle of incidence than cross-track

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Uncertainty Principle for radiometers

For a given integration time, , there is a trade-off between spectral resolution, B andradiometric resolution, T

For a stationary radiometer, make larger.

For a moving radiometer, is limited since it will also affect the spatial resolution. (next)

B

MT

M= figure of merit

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Airborne scanning radiometer

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Airborne scanning

Consider a platform at height h, moving at speed u, antenna scanning from angles s and –s , with beamwidth , along-track resolution, x

The time it takes to travel one beamwidth in forward direction is

The angular scanning rate is

The time it takes to scan through one beamwidth in the transverse direction is the dwell time

1

2

ts

Sd

t

21

u

xt

1

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Dwell time Is defined as the time that a point on the

ground is observed by the antenna beamwidth. Using

For better spatial resolution, small

For better radiometric resolution, need large

As a compromise, choose

hu

xt

ssd

22

21

hx

suhx 2

B

MT

d

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Radiometer Uncertainty Eq.

Equating, we obtain;

suhMBxT 2

Radiometric resolution

Spatial resolution

Spectralresolution

This equation applies for this specific scanning configuration.

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Problem 6.6 A 1GHz balanced Dicke radiometer with a 100 MHz

bandwidth is to be flown on a satellite at an altitude of 600 km with average speed of 7.5 km/s.

The radiometer uses a 10-m diameter antenna, and the receiver is characterized by T’rec=1000K and Tref=300K. Take antenna efficiency k=1.5 [k /l]

The radiometer integration time is chosen to be equal to 0.1 of the dwell time of the antenna beam for a point on the ground. If the antenna is fixed so that its main beam is always pointed in the nadir direction,

What will T be?

= 0.1678 K

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WindSat first images @ Ka