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Radiometer Systems

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Title: Radiometer Systems


1
Radiometer Systems
  • INEL 6669
  • microware remote sensing
  • S. X-Pol

2
Microwave Sensors
Radar (active sensor)
Radiometer (passive sensor)
3
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 (systems noise).

4
Topics of Discussion
  • Equivalent Noise Temperature
  • Noise Figure Noise Temperature
  • Cascaded System
  • Noise for Attenuator
  • Super-heterodyne Receiver
  • System Noise Power at Antenna
  • Radiometer Operation
  • Measurement Accuracy and Precision
  • Effects of Rx Gain Variations

5
Topics of Discussion
  • Dicke Radiometer
  • Balancing Techniques
  • Reference -Channel Control
  • Antenna-Channel Noise-Injection
  • Pulse Noise-Injection
  • Gain-Modulation
  • Automatic-Gain Control (AGC)
  • Noise-Adding radiometer
  • Practical Considerations Calibration Techniques

6
Radiometers 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 DT.

7
Noise voltage
  • The noise voltage is
  • the average0 and the rms is

8
Noisy resistor connected to a matched loadis
equivalent to ZL(RjX)R-jX
Independent of f and R!,
9
Equivalent Output Noise Temperature for any noise
source
TE is defined for any noise source when connected
to a matched load. The total noise at the output
is
10
Noise Figure, F
  • Measures degradation of noise through the device
  • is defined for To290K (62.3oF!, this winter in
    Puerto Rico.)

Total output signal Total output noise
Noise introduced by device
11
Noise Figure, F
  • Noise figure is usually expressed in dB
  • Solving for output noise power

12
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 To290K
    (room temperature)

75K
Examples 1dB NF is and 3dB NF is
What is TE for F2dB?
288K
170K
13
Cascade System
14
Noise of a cascade system
15
Noise for an Attenuator
16
Antenna, TL and Rx
17
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 IFltRF), 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.

18
Superheterodyne receiver
G23dB F7.5dB
RF amp Grf ,Frf ,Trf
IF amp Gif ,Fif ,Tif
Mixer GM,FM,TM
Pni
Pno
G30dB F2.3dB
G30dB F3.2dB
LO
Example Trf290(10.32-1)638K Tm1,340K Tif203K
TREC?
19
Equivalent System noise power at antenna terminals
  • Taking into consideration the losses at the
    antenna and T.L. with a physical temperature of
    Tp

20
Equivalent System noise power at antenna terminals
  • Then the total noise for the system is

For radiometer , Psys Prec For Radar, S/N
Pr/Psys
21
Summary
  • Antenna
  • Antenna losses
  • Receiver
  • Receiver T.L.
  • All of the above

22
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) DT

23
Total Power Radiometer
Super-heterodyne receiver uses a mixer, L.O. and
IF to down-convert RF signal. Usually BRFgtBIF
24
Detection- power spectra _at_
25
Noise voltage after IF amplifier
The instantaneous IF voltage has a time-varying
envelop ve(t) and phase angle f(t)
with zero average
The average IF power is equal to the average of
the square of vIF(t)
26
Noise voltage after detector, Vd
The detector voltage is proportional to the
square of the envelop voltage
Ve
Vd
27
Noise voltage after Integrator
Ve
  • For averaging the radiometer uses an Integrator
    (low pass filter). It averages the signal over an
    interval of time t with voltage gain gI.
  • Integration of a signal with bandwidth B during
    that time, reduces the variance by a factor NBt,
    where B is the IF bandwidth.

Vd
Vout
28
Radiometric Resolution, DT
Ve
Vd
  • The output voltage of the integrator is related
    to the average input power, Psys

Vout
GS is the overall system gain factor.
Which can be solved forTA
29
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.
    html
  • http//www.millitech.com/pdfs/Radiometer.pdf

30
The IF voltage
  • Is a sum of noise signals with same frequency
  • In phase-domain
  • Since summing Ns random noise sources, Ve has
    probability density function pdf given by (see
    section 5.7 Ulaby Long 2013)
  • With an associated standard-deviation
  • to mean ratio

Before integration
31
The detection voltage Vd has a DC component and
an AC component.
  • The DC component is proportional to the Tsys
  • The AC component are related to the fluctuations
    related to the statistical uncertainties of
    measurement.

Before integration the uncertainty is so large
that its equal to the signal we want to detect.
So we need to filter the AC AC component which
is equivalent to integrating (averaging) over
time.
32
Integration
  • Averaging over a B bandwidth and during t time,
    reduces the variance by a factor NBt
  • Total rms uncertainty

Still have fluctuations after LPF but are smaller
33
Radiometric Sensitivity
  • Since and
    then
  • The Noise-caused uncertainty
  • Its the minimum (statistically) detectable
    change in radiometric antenna temperature of the
    observed scene.

Radiometric Sensitivity (or resolution)
34
Total-power radiometer
  • This doesnt take into account variations in Gain
  • Its also known as
  • Where the bandwidth is called the predetection
    bandwidth and given a nonuniform transfer
    funcition is given by

Ideal total-power radiometer
35
Receiver Gain variations
  • DT is due to various causes
  • Noise-caused uncertainty
  • Gain-fluctuations uncertainty
  • Total rms uncertainty

Total-power radiometer resolution including gain
variations
Also, Try with 10-5 gain variation and no RF amp
(TREC3000K)
36
Gain Variations and the 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.

37
Dicke radiometer
Unity-gain amplifiers (-) ()
The radiometer voltage is
The switching rate is fs switching period ts is
much shorter than integration time.
38
Dicke Radiometer
Noise-Free Pre-detection Section Gain
G Bandwidth B
Switching rate, fs 1/ts
  • Dicke Switch
  • Synchronous Demodulator

Nyquist sampling theorem
39
Dicke radiometer
The radiometer switches rapidly between reference
and antenna using the Dicke switching
40
Dicke Radiometer resolution
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
41
Dicke radiometer resolution
  • The uncertainty in T due to noise when looking at
    the antenna or reference (half the integration
    time)
  • Unbalanced Dicke radiometer resolution

Example B100MHz, t1s, Trec 700K, DG/G.01,
Tref300K for TA0K and 300K, for Total P
radiometer and Dicke radiometer
42
Balanced Dicke
A balanced Dicke radiometer is designed so that
TA Tref at all times. In this case,
43
Balancing Techniques
  • Reference Channel Control
  • Antenna Noise Injection
  • Pulse Noise Injection
  • Gain Modulation
  • Automatic Gain Control

44
Reference Channel Control
Force TA T ref
Switch driver and Square-wave generator, fS
Vout ?
Pre-detection G, B, TREC
Vout
TA
Integrator t
Synchronous Demodulator
Tref
Measures vc
Feedback and Control circuit
Vc
Variable Attenuator at ambient temperature To
L
TN
Noise Source
45
Reference Channel Control
  • TN and To have to cover the range of values that
    are expected to be measured, TA
  • If 50kltTAlt 300K
  • Use To 300K and need cryogenic cooling to
    achieve TN 50K.
  • But L cannot be really unity, so need TN lt 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.

46
Cryogenic-cooled Noise Source
  • When a passive (doesnt 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 77.36K
  • Used on ground based radiometers, but not
    convenient for satellites and airborne systems.

47
Active cold or hot sources
  • http//www.maurymw.com/
  • http//sbir.gsfc.nasa.gov/SBIR/successes/ss/5-049t
    ext.html

48
Active noise source FET
  • The power delivered by a noise source is
    characterized using the ENRexcess noise ratio
  • where TN is the noise temperature of the source
    and To is its physical temperature.

Example for 9,460K ENR 15 dB
49
Antenna Noise Injection
Measures vc
Force TA T ref T o
TN
Variable Attenuator
Fc Coupling factor of the
directional coupler
50
Antenna Noise Injection
  • Combining the equations and solving for L
  • from this equation, we see that To should be gtTA
  • If the control voltage is scaled so that Vc1/L,
    then Vc will be proportional to the measured
    temperature,

51
Example Antenna Noise Injection
Find the necessary values of the Attenuator L, to
measure this range of Temperatures and the
resolution for this balanced Dicke radiometer
given
Choose To310K
52
Example Antenna Noise Injection
  • If 50Klt TAlt 300K, need to choose Togt300K, say
    To310K
  • If Fc100(20dB) and Tn50,000K
  • Find L variation needed

53
Antenna Noise InjectionResolution
  • For expected measured values between 50K and
    300K, Tref is chosen to be To310K, so
  • Since the noise temperature seen by the input
    switch is always To , the resolution is

54
Pulse Noise Injection
Measures fr
Switch driver and Square-wave generator, fS
TA
Vout
TA
Coupler
Pre-detection G, B, Trec
Integrator t
Synchronous Demodulator
TN
Tref
Feedback and Control circuit
f r
Pulse- Attenuation Diode switch
Noise Source
TN
55
Pulse Noise Injection
  • Reference T is controlled by the frequency of a
    pulse
  • The repetition frequency is given by

56
Pulse Noise Injection
Ton
Pulse repetition frequency fR 1/tR Pulse
width is constant tp Square-wave modulator
frequency fSlt fR/2
Toff
Switch ON minimum attenuation Switch Off
Maximum attenuation
ExampleFor Lon 2, Loff 100, tp 40 ms, To
300K and TN 1000K, F20dB
We obtain Ton 650K, Toff 307K
57
Example Pulse Noise-Injection
  • With

58
Summary
59
Summary
60
Cont Source Microwave Radiometer Resolution
Optimization Using Variable Observation Times,
by Adriano Camps and Jose Miguel Tarongí
61
Gain-Modulation
Measures vc
Switch driver and Square-wave generator, fS
TA
Fixed attenuator Lo
Synchronous Demodulator
Pre-detection G, B, Trec
Tref
Variable attenuator Lv
v c
Integrator t
Control circuit
Vout
Drawback slow variations of receiver noise
temperature, yields error in reading.
62
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.

63
Automatic Gain-Control (AGC)
Switch driver and Square-wave generator, fS
2fs
Synchronous Demodulator 2fs
Pre-detection G, B, Trec
gv
Reference Switch
Integrator t
Synchronous Demodulator fs
fs
T2
Gv
T1
Feedback amplifier
Vagc
Hach radiometer insensitive to variations from
G, and Trec.
64
Dicke Switch
  • Two types
  • Semiconductor diode switch, PIN
  • Ferrite circulator
  • Switching rate, fS ,
  • High enough so that GS remains constant over one
    cycle.
  • To satisfy sampling theorem, fS gt2BLF
  • http//envisat.esa.int/instruments/mwr/descr/chara
    ct.html

65
Dicke Input Switch
  • Important properties to consider
  • Insertion loss
  • Isolation
  • Switching time
  • Temperature stability

http//www.erac.wegalink.com/members/DaleHughes/My
EracSite.htm
66
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 on satellites
  • use outer space 2.7K
  • http//ipnpr.jpl.nasa.gov/progress_report/42-154/1
    54G.pdf

67
Imaging Considerations
  • Scanning configurations
  • Electronic (beam steering)
  • Phase-array (uses PIN diode or ferrite
    phase-shifters, are expensive, lossy)
  • Frequency controlled
  • Mechanical (antenna rotation or feed rotation)
  • Cross-track scanning
  • Conical scanning (push-broom) has less variation
    in the angle of incidence than cross-track

68
Uncertainty Principle for radiometers
M figure of merit
  • For a given integration time, t, there is a
    trade-off between
  • spectral resolution, B and
  • radiometric resolution, DT
  • For a stationary radiometer, make t larger.
  • For a moving radiometer, t is limited since it
    will also affect the spatial resolution. (next)

69
Airborne scanning radiometer
70
Airborne scanning
  • Consider a platform at height h, moving at speed
    u, antenna scanning from angles qs and qs , with
    beamwidth b, along-track resolution, Dx
  • The time it takes to travel one beamwidth in
    forward direction is
  • The angular scanning rate is
  • The time it stays while scanning through one (1)
    beamwidth in the transverse direction is the
    dwell time

71
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 t
  • For better radiometric resolution, need large t
  • As a compromise, choose

72
Radiometer Uncertainty Eq.
  • Equating, we obtain

Radiometric resolution
This equation applies for this specific scanning
configuration.
Spatial resolution
Spectral resolution
73
Problem
  • 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 Trec1000K and
    Tref300K. Take antenna efficiency k1.5 b?k
    l/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 DT be?

0.1678 K
74
WindSat first images _at_ Ka
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