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Microwave Remote Sensing Principles and Applications

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Microwave Remote Sensing: Principles and

Applications

• Outline

– Introduction to RSL at the University of Kansas

– Introduction and History of Microwave Remote Sensing

– Active Microwave Sensors

• Radar Altimeter.

• Scatterometer.

• Imaging Radar.



– Applications of Active Sensors



• Sea ice.

• Glacial ice

• Ocean winds.

• Soil Moisture.

• Snow.

• Vegetation.

• Precipitation.

• Solid Earth.







11/18/02 University of Kansas

Microwave Remote Sensing: Principles and

Applications



• Passive Microwave Sensors

– Radiometers

• Traditional

• Interferometer

• Polarimetric Radiometer

• Application of Passive Microwave Sensors

• Sea ice.

• Glacial ice

• Soil Moisture.

• Atmospheric sounding

• Snow.

• Vegetation.

• Precipitation



11/18/02 University of Kansas

Radar Systems and Remote Sensing

Laboratory

Windvector

Measurements over

the Ocean

Radar at 14 GHz.

Concept developed at

KU.

USA, Europe and

Japan are planning

to launch satellites

to obtain data

continuously.



11/18/02 University of Kansas

Radar Systems and Remote Sensing

Laboratory

Founded in 1964.

4 Faculty members, 20 Graduate students - Ph. D & M.S.

4-6 Undergraduate students, 2 Staff

Now satellites based on concepts developed at RSL are in

operation.

NSCAT, QUICKSCAT- Radars to measure ocean surface winds.

ADEOS-2 (JAPAN), Europeans Met Office is planning to launch

satellite to support operational applications.

ScanSAR-

Radarsat- Canadian satellite

Envisat - European

SRTM -Shuttle Radar Topography Mission.Radar Systems

and Remote Sensing Laboratory







11/18/02 University of Kansas

Radar Systems and Remote Sensing

Laboratory

• Shuttle Radar Topography

Mission (SRTM)

– to collect three-

dimensional

measurements of the

Earth's surface.

– Acquired data to obtain

the most complete

near-global mapping of

our planet's topography

to date.

– This would not have

been possible without

ScanSAR operation---

concept developed at

KU.





11/18/02 University of Kansas

ITTC– Information Technology &

Telecommunication Center

• Communications academic emphasis and

research programs established in 1983.



• Now RSL is a part of the Center

• Graduated students

– degrees in EE, CS, CoE, Math

• 29 faculty, 15 staff researchers, 6 Center

staff

• Current student population ~ 130

– ~ 13 Ph.D., ~81 M.S., ~37 B.S.







11/18/02 University of Kansas

EM Spectrum



• Microwave region

• 300 MHz – 30 GHz.

Millimeter wave

• 30 GHz – 300 GHz.



IEEE uses a different

definition

• 300 MHz – 100 GHz









11/18/02 University of Kansas

Microwave Remote Sensing: Principles and

Applications.



• Advantages

– Day/night coverage.

– All weather except during

periods of heavy rain.

– Complementary

information to that in

optical and IR regions.

• Disadvantages

– Data are difficult to

interpret.

– Coarse resolution except

for SAR.



11/18/02 University of Kansas

Microwave Remote Sensing— history



• US has a long history in Microwave Remote Sensing.

– Clutter Measurement program after the WW-II.

• Ohio State University collected a large data

base of clutter on variety of targets.



– Earnest studies for the remote sensing of the

earth can be considered to have began 1960s.

• In 1960s NASA initiated studies to investigate

the use of microwave technology to earth

observation.



11/18/02 University of Kansas

Microwave Remote Sensing— history



• The research NASA and other agencies initiated resulted in:



– Development of ground-based and airborne sensors.

– Measurement of emission and scattering characteristics of

many natural targets.

– Development of models to explain and understand measured

data.

– Space missions with microwave sensors.

• NIMBUS

– Radiometers.

• SKYLAB

– Radar and Radiometers







11/18/02 University of Kansas

Microwave Remote Sensing



• Radar Applications

– Radio Detection and

Ranging. Civilian

Military

Navigation and Navigation and

– Texts: tracking tracking



• Skolnik, M. I., Search and

Search and

Introduction to Radar

surveillance

surveillance

Systems, McGraw Hill, Imaging &

1981. Mapping Imaging &

Mapping

• Stimson, G. W., Weather

Introduction to Airborne Sounding Weather

Radar, SciTech Probing

Publishing, 1998. Proximity fuses

Remote sensing

Counter measures







11/18/02 University of Kansas

Review – EM theory and Antennas



• Propagation of EM  H  J 

D

waves is governed by t

Maxwell equations.  E  

B

t

.B  0

• For time-harmonic

variation we can .D  

write the above   H  J  j E

equations as   E   j H

.B  0

.D  

11/18/02 University of Kansas

EM Theory



• Helmholtz Equation  E  2E  0

2









– From the four  H  2 H  0

2







Maxwell equations, where   

we can derive vector

Helmholtz equations  2 Ex  2 Ex  2 Ex

    2 Ex  0

x 2

y 2

z 2





2Ey 2Ey 2Ey

– For each component     2Ey  0

x 2

y 2

z 2



of E and H field we

 2 Ez  2 Ez  2 Ez

can write a scalar x 2



y 2



z 2

  2 Ez  0

equation





11/18/02 University of Kansas

Uniform plane wave



Amplitude and phase are constant on

planes perpendicular to the direction of

propagation.

TEM case– no component in the direction

of propagation.

For a TEM wave propagating in z direction

Ez = 0 and Hz =0

Ex(z,t) = Eo e-αz Cos(ωt-jβz)

11/18/02 University of Kansas

EM theory



• α and β are     j  j   j

determined by For a loss - loss medium   

material properties. 

 

2 

   

• Materials are r

Fresh wate ice, dry snow and



classified as dry soil are examples of low - loss media.

For a conductor  

insulators and 

conductors   

2





11/18/02 University of Kansas

EM Theory



• Reflection and

refraction θi θr

– Whenever a wave

impinges on a

dielectric interface, θt

part of the wave will

be reflected and

remaining will be

transmitted into the

lower medium.





11/18/02 University of Kansas

EM Theory--Scattering





• Microwave Scattering from a

distributed target depends on

– Dielectric constant.

– Surface roughness.

– Internal structure.

• Homogeneous

• Inhomogeneous

– Wavelength or Frequency.

– Polarization.

11/18/02 University of Kansas

Microwave Scattering



• Surface scattering θi

θr

– A surface is classified as

smooth or rough by

comparing its surface Smooth surface

height deviation with

wavelength.

• Smooth h 2 fdmax For a radar withf p  1500 Hz

3x108

R un   100 km

2 x1500

c p

r  , r  150m for  p  1 s

2









11/18/02 University of Kansas

Radar—Principle



• Radar equation • For a monostatic radar

• GT = GR

PT • Radar sensitivity is determined

by the minimum detectable

GT R signal set by the receiver noise.

• No = kTBF

Power density at the target is given byP

PG

• F= noise figure

Pd  T T



• Signal-to-noise ratio

4R 2

Target with radar crosssection, , intercepts

a part of this signal and reradiates

in the direction of the radar.

PG

Pdr  T T 

4R 2 S P P T GT 2

2

 r 

N N o ( 4 ) 3 R 4 KTBF

Reradiated power incident on the antenna is given by

PG 1

Pri  T T 

4R 2 4R 2

The receive antenna with an effectiveaperture, Ae, incident signal and it is given by P T GT2 2

PG Ae Rm ax  1

Pr  T T  4 S

4R 2 4R 2 (4 ) 3 KTBF

P G G 2 N

Pr  T T 3R 4

(4 ) R

4A

where GR  2 e











11/18/02 University of Kansas

Microwave Remote Sensing



• Radar cross section

characterizes the 2

size of the object as

Es

  Lim R  4R 2



seen by the radar.

2

Ei

Where

Es = scattering field

Ei = incident field

r   r 2









11/18/02 University of Kansas

Radar Equation



• A distributed target   oA



contains many  o  scattering coefficient





scattering centers

A  Illu min ated area



P T GT 2 0 A

2



within the Pr 

(4 ) 3 R 4

illuminated area. It e a



is characterized by o

R

radar cross section

per unit area, which

is refereed to as      

scattering

A 

R cos( 0 ) tan( o  e )  tan( o  e )  R tan( a )

2  2 2  2

If  0  1 &   1

coefficient A



R2e a

4





11/18/02 University of Kansas

Radar Equation



P T GT 2 0 R e R a

2

Pr 

( 4 ) 3 R 4 4

P T GT 2 0  e  a

2

Pr 

( 4 ) 2 R 2 16



For a distributed power received falls off as 1/R2



For a point target power received falls off as 1/R4









11/18/02 University of Kansas

Antenna Array

R1  Ro  d sin  





• Let us consider

R  d sin  

2

  d sin  





simple array   j 2R0

Et  Eo  e   e





j

2 ( Ro  d sin  















consisting of

d sin  

j

2R0

j  j d sin    j d sin   

Et  Eo e 

e  e   e  

 

 





isotropic radiators.

j

2R0

j

d sin  )

d sin  

Et  2 Eo e 

e 

cos )



 2d sin   

Et   Eoi cos 

i   

R1 If we increase from 0 to 90 degrees

and reduce the resulting expression.

sinx

Et 

x

Ro

d











P

11/18/02 University of Kansas

Antenna Array

R1  Ro  d sin  





• Let us consider

R  d sin  

2

  d sin  





simple array   j 2R0

Et  Eo  e   e





j

2 ( Ro  d sin  















consisting of

d sin  

j

2R0

j  j d sin    j d sin   

Et  Eo e 

e  e   e  

 

 





isotropic radiators.

j

2R0

j

d sin  )

d sin  

Et  2 Eo e 

e 

cos )



 2d sin   

Et   Eoi cos 

i   

R1 If we increase from 0 to 90 degrees

and reduce the resulting expression.

sinx

Et 

x

Ro

d











P

11/18/02 University of Kansas

Microwave Remote Sensing: Principles and

Applications— History



• Active Microwave sensing

– Studies related to active sensing of the

earth beagn in 1960s.

• Clutter studies

• SkYLab – radar altimeter and scatterometer in

1960s

• SEASAT in 1978

• ERS-1, JERS-1, ERS-2, RADARSAT, GEOSAT,

Topex-Posoidon





11/18/02 University of Kansas

Active Sensors – Radar Altimeter





• Radar altimeter is a short pulse radar

used for accurate height measurements.

– Ocean topography.

– Glacial ice topography

– Sea ice characteristics

• Classification and ice edge

• Vegetation

•http://topex-www.jpl.nasa.gov/technology/images/P38232.jpg









11/18/02 University of Kansas

Radar Altimeter



• Missions

Satellite Radar Altimeters

Mission Frequency Accuracy Period

SKYLAB Ku 10 m 1973



GEOS Ku 1-5 M 1976

SEASAT Ku ~1 m 1978

GEOSAT Ku 10 CM 1985-1990

ERS-1 Ku < 10 cm 1992-1998

TOPEX C &Ku < 10 cm 1992-

ERS-2 Ku < 10 cm 1996-

GFO Ku <10 cm 1998-

ENVISAT Ku &S <10 CM 2001-

Jason-1 Ku &C <10 cm 2000-

CRYOSAT and other

missions Ku Few cm 2003-







11/18/02 University of Kansas

Radar Altimeter— Waveform



• Satellite altimeters operate

in pulse-limited mode.

R2  H 2  Y 2

c

RH H



2

c 

2



H    H Y

2 2 Ct/2





 2 

c

 H

2

c

H 2  cH  ( ) 2  H 2  Y 2

2

Y  cH

R  Re solution  2Y  2 cH

Amplitude

For H  800 km,  3.3 ns

R  1.7km

Time









11/18/02 University of Kansas

Radar Altimeter



• A short pulse radar

– Uses pulse compression to obtain fine range

resolution or height measurement.

– Range measurement uncertainty of a pulse radar.



c

r  

S

2B 2

N

For example B  300 MHz, S/N  100

r  3.5 cm



11/18/02 University of Kansas

Radar altimeter



• Other sources of errors

– Atmospheric delays

– Troposheric delays.

– EM bias

– Pointing errors

– Orbit errors

– Accuracies of few cms are

being achieved with new

generation sensors.

• Dual-frequency

• Water vapor— Resti et al, “The Envisat Altimeter System RA-2,”ESA

radiometers Bulletin 98, June 1999



• GPS – orbit determination

• Calibration.

sigma=5.5 cm









11/18/02 University of Kansas

Radar Altimeter—typical system









Resti et al, “The Envisat Altimeter System RA-2,”ESA Bulletin 98, June 1999







11/18/02 University of Kansas

Radar Altimeter



• Waveform analysis

– Time delay is measured

very accurately and

converted into

distance.

– Spreading of the pulse

is related to SWH.

– Scattering coefficient

can be obtained by

determining the power.



Resti et al, “The Envisat Altimeter System

RA-2,”ESA Bulletin 98, June 1999





11/18/02 University of Kansas

Radar Altimeter- typical system



• Block diagram of Envisat RA









Resti et al, “The Envisat Altimeter System RA-2,”ESA Bulletin 98, June 1999







11/18/02 University of Kansas

Active sensors



• Scatterometer

– Scatter o Meter – A calibrated radar used to

measure scattering coefficient.

– They are used to measure radar backscatter as a

function of incidence angle.

– Ground and aircraft-based scatterometers are

widely used.

– Experimental data on variety of targets to support model

and algorithm development activities.

» Developing algorithms for extracting target

characteristics from data.

» Understanding the physics of scattering to develop

empirical or theoretical models.

» Developing target classification algorithms





11/18/02 University of Kansas

Active sensors— Scatterometers



• Wide range of applications

– Wind vector measurements

– Sea and glacial ice

– Snow extent.

– Vegetation mapping

– Soil moisture

• Semi-arid or dry areas.







11/18/02 University of Kansas

Microwave Remote Sensing— Atmosphere

and Precipitation



• Global precipitation mission

– Will consist of a primary spacecraft and a

constellation.

• Primary Spacecraft

– Dual-frequency radar.

» 14 and 35 GHz.

– Passive Microwave Radiometer





– Constellation Spacecraft

• Passive Microwave Radiometer



11/18/02 University of Kansas

Microwave Remote Sensing—Active

Sensors



Imaging Radars

Imaging Radars & Scatterometers





• Imaging Radars

• Real Aperture Radar (RAR)

• Synthetic Aperture Radar (SAR)

• Widely used for military and civilian

applications.

• RAR

• Thin long antenna mounted on the side of an

aircraft.







11/18/02 University of Kansas

Imaging radars



• RAR • RAR geometry

– Resolution is

determined by

antenna beamwidth in

the along track

direction r  R  k

a

R

D

a





k  weighting factor





– Pulse width in the

cross-track direction

c

rc 

2 sin( )









11/18/02 University of Kansas

Imaging radars



• For a radar operating

at f=10 GHz with a 3-m 10000x0.03

ra  0.8  80 m

long antenna in the 3

along track direction rc 

3x108 x0.5 x106

 106 m

and 0.5 us pulse, 2 sin(45)

R  100 km

resolution at 45 degree

100000x0.03

incidence and range of ra  0.8

3

 800 m

10 km is given by 3x108 x0.5 x106

rc   106 m

• Assume k=0.8 2 sin(45)









11/18/02 University of Kansas

Imaging Radars: RAR



RARs were used

• Resolution until 1990s.

They are replaced

by SARs.

Resolution should

1/20 about the

dimensions of the

target we want to

recognize

MRS: vol. II, Ulaby, Moore and Fung



11/18/02 University of Kansas

SAR



• Synthetic Aperture Radar

• Use the forward motion of an aircraft or a

spacecraft to synthesize a long antenna.

• Satellite SARs

• ERS-1, ERS-2, RADARSAT, ENVISAT, JERS-1,

SEASAT, SIR-A,B& C.

• Applications

• Ocean wave imaging

• Oil slick monitoring

• Sea ice classification and dynamics

• Soil moisture

• Vegetation

• Glacial ice surface velocity







11/18/02 University of Kansas

SAR





• We can use a small physical antenna

• For focused SAR resolution is

independent of

• Wavelength

• Range

• Best possible resolution is L/2

• Where L= length of the physical antenna





11/18/02 University of Kansas

RF Spectrum



Microwave Radiometry covers a range of frequencies.



Soil Atmospheric

Atmospheric

Moisture Ocean Surface Wind Water Vapor Cloud Ice

Temperature

1-3 GHz 19, 22 GHz 22, 24, 92, 150, 325, 448, 643 GHz

54, 118 GHz

Resolution / Polarimetry 183 GHz High frequency

Accuracy

aperture Accuracy









 30 cm 3 cm 3 mm 0.3 mm







 1 GHz 10 GHz 100 GHz 1000 GHz









Atmospheric

Sea Surface Salinity Precipitation

Sea Ice Chemistry

1-3 GHz 11, 31,37,89 GHz

37 GHz 190, 240, 640,

Receiver sensitivity/ Frequent global

Polar coverage 2500 GHz

stability coverage

High frequency



Hartley, NASA

L band S band C band X band Ku/K/Ka band Millimeter Submillimeter

11/18/02 University of Kansas

Microwave Radiometers— theory



• Planck’s Law of radiation

2hc 2 1

s ( , T ) 

 5 ch



e kT

1



• Where S(λ,T) =Intensity of

radiation in w/m2

• T = temperature in Kelvins

• h = Planck’s constant, 6.625 ×

10-34 J·s Rayleigh  Jeans Approx



• c = velocity of propagation

ch

 kT





m/s

2ckT

S ( , T ) 

4





• k = Boltzmann constant,

1.380 × 10-23 J/K

• λ = wavelength, m





11/18/02 University of Kansas

Microwave Radiometer



• At microwave frequencies radiation

intensity is directly proportional to the

temperature.

• For gray bodies

– Pa = kTb B

– k =Boltzman constant, B = bandwidth, Hz.

– Tb = Brightness temperature, K

– Tb =e Tphy

– e = Emissivity of the object or media

11/18/02 University of Kansas

Microwave Radiometer



Two basic types of radiometers

– Total power radiometer

• Highest sensitivity

– Switching-type radiometers and its variants.

TTotal

T 

B in

• Typical total power radiometer where Ttota l  Ta  Tsy s

B bandwidth

Mixer

Square-law det  in  int egration time

LNA IF Amp

Bandpass Filter Integrator

B  6 MHz, in  1s

Ttotal  500 K

Local Oscillator

T  0.2 K

11/18/02 University of Kansas

Microwave Radiometer



• Dicke or Switching-type radiometer

– Any fluctuations in gain of the receiver will

reduce radiometer sensitivity.

– To eliminate system effects, Dicke

developed switching type radiometer.

• It consists of switch and a synchronous

detector. The input is switched between the

antenna and noise source. If the injected noise

power is equal to input signal power, the effect

of gain fluctuations is eliminated.



11/18/02 University of Kansas

Microwave Radiometer



• Typical Dicke-type radiometer

Modulator







Mixer Bandpass Filter

-

LNA Diff Amp

+

L IF Amp +



Noise

source





Local Oscillator





If the duty cycleis 50%, integration time is reduced by 50%

1.4Ttotal

T 

B in









11/18/02 University of Kansas

RF Radiometry Characteristics



Moden Radiometer

Digital processor

To eliminate down conversion process



Antenna

Receiver



digital

multiplexer/ detector/

low noise mixer processor/

spectrometer digitizer

amplifier correlator



LO

Hartley, NASA

scan



11/18/02 University of Kansas

Microwave Remote Sensing



• Research and application of

microwave technology to remote

sensing of

– Oceans and ice

– Solid earth and Natural hazards..

– Atmosphere and precipitation.

– Vegetation and Soil moisture

11/18/02 University of Kansas

Microwave Remote Sensing— Ocean and

Ice

• Winds

– Scatterometer.

• Quickscat, Seawinds

– Polarimetric radiometer

• Ocean topography

– Radar altimeters

• Ocean salinity

– AQUARIUS

• Radiometer and radar combination.

– Radar to measure winds for correcting for the effect

of surface roughness.





11/18/02 University of Kansas

Ocean Vector Winds— Scatterometers









Scatterometers send microwave pulses to the

Earth's surface, and measure the power scattered

back. Backscattered power over the oceans

SeaWinds

depends on the surface roughness, which in turn

QuikScat

depends on wind speed and direction.

QuikScat

• Replacement mission for NSCAT, following loss of ADEOS

• Launch date: June 19, 1999

SeaWinds

• EOS instrument flying on the Japanese ADEOS II Mission

• Launch date: December 14, 2002 ????

Instrument Characteristics of QuikScat and SeaWinds

• Instrument with 120 W peak (30% duty) transmitter at 13.4

GHz, 1 m near-circular antenna with two beams at 46o and 54o

incidence angles









Advanced sensors– larger aperture

antennas.Passive polarimetric sensors.

11/18/02 University of Kansas

Courtesy: Yunjin Kim, JPL

Ocean Topography Missions









The most effective measurement of ocean currents

from space is ocean topography, the height of the sea

surface above a surface of uniform gravity, the geoid.



TOPEX/Poseidon and Jason-1

• Joint NASA-CNES Program

– TOPEX/Poseidon launched on August 10, 1992

– Jason-1 launched on December 7, 2001

• Instrument Characteristics

– Ku-band, C-band dual frequency altimeter

– Microwave radiometer to measure water vapor

– GPS, DORIS, and laser reflector for precise orbit determination

• Sea-level measurement accuracy is 4.2 cm

• TOPEX/Poseidon & Jason-1 tandem mission for high resolution ocean

topography measurements







The priority is to continue the measurement

with TOPEX/Poseidon accuracy

on a long-term basis for climate studies.

Courtesy: Yunjin Kim, JPL TOPEX/Poseidon Ocean topography

11/18/02 University of Kansas of the Pacific Ocean during El Niño

and La Niña.

Ocean Surface Topography Mission

An Experimental Wide-Swath Altimeter



By adding an interferometric radar system to a conventional radar altimeter

system, a swath of 200 km can be achieved, and eddies can be monitored over

most of the oceans every 10 days. The design of such a system has

progressed, funded by NASA’s Instrument Incubator Program. This

experiment is proposed to the next mission, OSTM (Ocean Surface

Topography Mission)









South America

Courtesy: Yunjin Kim, JPL



11/18/02 University of Kansas

Global Ocean Salinity





• Aquarius (JPL, GSFC, CONAE)

• ESSP-3 mission in the risk

mitigation phase

• First instrument to measure global

ocean salinity

– Passive and active microwave

instrument at L-band

– Resolution

• Baseline 100km, Minimum 1 week of salinity measurements from space

200km

– Global coverage in 8 days

– Accuracy: 0.2 psu

– Baseline mission life: 3

years









11/18/02 University of Kansas

Courtesy: Yunjin Kim, JPL 100 yrs of salinity measurements by ship

SRTM (Shuttle Radar Topography Mission)





• C-band single pass interferometric SAR for

topographic measurements using a 60m

mast

• DEM of 80% of the Earth’s surface in a

single 11 day shuttle flight

– 60 degrees north and 56 degrees south

latitude

– 57 degrees inclination

• 225 km swath

• WGS84 ellipsoid datum

• JPL/NASA will deliver all the processed data

• Partnership between NASA and NIMA to NIMA by January 2003

(National Imagery and Mapping Agency) • Absolute accuracy requirements

•X-band from German and Italian space – 20 m horizontal

agencies – 16 m vertical

• The current best estimate of the SRTM

accuracy is

Courtesy: Yunjin Kim, JPL

• 10 m horizontal and 8 m vertical

11/18/02 University of Kansas

L-band InSAR Technology





• Interferometric Synthetic Aperture Radar

(InSAR) can measure surface

deformation (mm-cm scale) through

repeated observations of an area

• L-band is preferable due to longer

correlation time due to longer

wavelength (24cm) Surface deformation due to Hector Mine

• Solid Earth Science Working Group Earthquake using repeat-pass InSAR data

recommended that

• In the next 5 years, the new space

mission of highest priority for solid-

Earth science is a satellite

dedicated to InSAR measurements

of the land surface at L-band





InSAR velocity difference indicates a 10%

increase in ice flow velocity from 1996 to

2000 on Pine Island Glacier

11/18/02 University of Kansas [Rignot et al., 2001]

Microwave Remote Sensing— Soil

Moisture.

Southern Great Plains Hydrology Experiment (SGP97)

Surface Soil Moisture Derived From Remotely Sensed Microwave Data

37.0

June 30 July 1





Radar

Lamont Lamont



36.5

Soil Moisture (%)

50

50





Pol: VV, HH & HV

36.0





ElReno ElReno

35.5 OklahomaCity OklahomaCity

40

40



Chickasha Chickasha









Res – 3 and 10 km









Latitude (Degrees)

35.0









SGP’97

30

30



July 2 July 3

Lamont Lamont





36.5

20

20



Radiometer 36.0





ElReno ElReno

10

10

OklahomaCity OklahomaCity

35.5







Pol: H, V 35.0

Chickasha Chickasha



00





-98.5 -98.0 -97.5 -98.0 -97.5 -97.0

Longitude (Degrees)



Res =40 km, NASA Land Surface Hydrology Program









dT= 0.64º K Courtesy: Tom Jackson, USDA







• HRDROS

– Back-up ESSP mission for global soil moisture.

• L-band radiometer.

• L-band radar.

11/18/02 University of Kansas

Microwave Remote Sensing— Atmosphere and

Precipitation CloudSAT



Salient Features

NASA ESSP mission

First 94 GHz radar space borne system

Co-manifested with CALIPSO on Delta launch vehicle

Flies Formation with the EOS Constellation

Current launch date: April 2004

Operational life: 2 years

Partnership with DoD (on-orbit ops), DoE

(validation) and CSA (radar development)





Science

Measure the vertical structure of clouds and quantify their ice and water content

Improve weather prediction and clarify climatic processes.

Improve cloud information from other satellite systems, in particular those of Aqua

Investigate the way aerosols affect clouds and precipitation

Investigate the utility of 94 GHz radar to observe and quantify precipitation, in the

context of cloud properties, from space

11/18/02 University of Kansas

Courtesy: Yunjin Kim, JPL

Earth Science and RF Radiometery







Atmospheric chemistry







Precipitation

Microwave Sea surface temperature/

Radiometry Sea surface salinity



Applications.

Hartley, NASA









Ocean surface wind

Atmospheric temperature, humidity, and clouds Soil moisture

11/18/02 University of Kansas

Conclusions



• A brief overview of microwave remote

sensing principles and applications.

• Opportunities for research and

education.

– Science

– Technology









11/18/02 University of Kansas

SAR—Principle



• SAR can explained using the concept

of a matched filter or antenna array.







Ro









11/18/02 University of Kansas

SAR— Principle



• Unfocussed SAR

4Ro

• No phase corrections are made. o 



4R

N 



2

l l2

R  R0     Ro 

2



Ro  2 8 Ro

4l 2 

 d   N  o  

r 8 Ro  4

Ro 

l

2









11/18/02 University of Kansas

SAR— Principle



• Focussed SAR

0.5

 x2 

R R 

 x 2  Ro 1  2 

2

o  R 

x x 2

 o 





R  Ro 

2 Ro

Ro 2 x2 2x 2

d ( x)  2 

 2 Ro Ro

2x 2

e

Thus we need to correct th phase by -

Ro

to make all the vectorsadd up









11/18/02 University of Kansas

SAR— Principle



• Resolution



The 3 - dB beamwidth of an uniformly illuminate d real



aperture of length, D, is given by  ar  0.88

D



For synthetic aperture of length, Leff ,  as  0.44

Lef

4 - dB beamwidth are given by

  Ro

 ar  ,  as  0.5 & Lef 

D Lef D

Ro D

Along track resolution, ra   as Ro  

2 Le f 2









11/18/02 University of Kansas


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