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Title: Active%20Microwave%20Remote%20Sensing


1
Active Microwave Remote Sensing
  • Lecture 9

2
Recap passive and active RS
  • Passive uses natural energy, either reflected
    sunlight (solar energy) or emitted thermal or
    microwave radiation.
  • Emitted microwave radiation can be all weathers
    capability
  • Active sensor creates its own energy
  • Transmitted toward Earth or other targets
  • Interacts with atmosphere and/or surface
  • Reflects back toward sensor (or backscatter)
  • Radar can be all weathers capability, Lidar for
    land surface still be affected by cloud and rain.

3
Widely used active RS systems
  • RADAR RAdio Detection And Ranging
  • Long-wavelength microwaves (1 100 cm)
  • LIDAR LIght Detection And Ranging
  • Short-wavelength laser light (UV, visible, near
    IR)
  • SONAR SOund Navigation And Ranging (very long
    wave, low Hz)
  • Sound can not travel through vacuum, so acoustic
    energy is not EMR energy
  • Earth and water absorb acoustic energy far less
    than EMR energy
  • Seismic survey use small explosions, record the
    reflected sound
  • Medical imaging using ultrasound
  • Sound waves can pass through a water column.
  • Sound waves are extremely slow (300 m/s in air,
    1,530 m/s in sea-water)
  • Bathymetric sonar (measure water depths and
    changes in bottom topography )
  • Imaging sonar or sidescan imaging sonar (imaging
    the bottom topography and bottom roughness)

4
Types of radar
  • Nonimaging radar
  • Traffic police use handheld Doppler radar system
    determine the speed by measuring frequency shift
    between transmitted and return microwave signal
  • Plan position indicator (PPI) radars use a
    rotating antenna to detect targets over a
    circular area, such as NEXRDA
  • Satellite-based radar altimeters (low spatial
    resolution but high vertical resolution)
  • Imaging radar
  • Usually high spatial resolution,
  • Consists of a transmitter, a receiver, one or
    more antennas, GPS, computers

5
Microwaves
Band Designations (common wavelengths
Wavelength (?) Frequency (?) shown in
parentheses) in cm in
GHz ______________________________________________
_ Ka (0.86 cm) 0.75 - 1.18 40.0 to 26.5 K 1.18
- 1.67 26.5 to 18.0 Ku 1.67 - 2.4 18.0 to
12.5 X (3.0 and 3.2 cm) 2.4 - 3.8 12.5 - 8.0 C
(7.5, 6.0 cm) 3.8 - 7.5 8.0 - 4.0 S (8.0,
9.6, 12.6 cm) 7.5 - 15.0 4.0 - 2.0 L (23.5,
24.0, 25.0 cm) 15.0 - 30.0 2.0 - 1.0 P (68.0
cm) 30.0 - 100 1.0 - 0.3
6
Two imaging radar systems
  • In World War II, ground based radar was used to
    detect incoming planes and ships (non-imaging
    radar).
  • Imaging RADAR was not developed until the 1950s
    (after World War II). Since then, side-looking
    airborne radar (SLAR) has been used to get
    detailed images of enemy sites along the edge of
    the flight field. The longer the antenna (but
    there is limitation), the better the spatial
    resolution. SLAR can be either a RAR or a SAR.
  • Real aperture radar (RAR)
  • Aperture means antenna
  • A fixed length (for example 1 - 15m)
  • Synthetic aperture radar (SAR)
  • 1m (11m) antenna can be synthesized
    electronically into a 600m (15 km) synthetic
    length.
  • Most (air-, space-borne) radar systems now use
    SAR.

7
Operating Principle of SLAR
waveform
8
Radar Nomenclature and Geometry
Radar Nomenclature nadir azimuth (or flight)
direction look (or range) direction range
(near, middle, and far) depression angle (?)
incidence angle (?) altitude above-ground-level,
H polarization
Azimuth flight direction
Look/Range direction
?
Flightline groundtrack
?
Near range
Far range
9
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10
Slant-range vs. Ground-range geometry
Radar imagery has a different geometry than that
produced by most conventional remote sensor
systems, such as cameras, multispectral scanners
or area-array detectors. Therefore, one must be
very careful when attempting to make
radargrammetric measurements. Uncorrected
radar imagery is displayed in what is called
slant-range geometry, i.e., it is based on the
actual distance from the radar to each of the
respective features in the scene. It is
possible to convert the slant-range display into
the true ground-range display on the x-axis so
that features in the scene are in their proper
planimetric (x,y) position relative to one
another in the final radar image.
11
  • Most radar systems and data providers now provide
    the data in ground-range geometry

12
Range (or across-track) Resolution
Pulse duration (t) 0.1 x 10 -6 sec
  • t.c called pulse length. The short pulse length
    will lead fine range resolution.
  • However, the shorter the pulse length, the less
    the total amount of energy that illuminates the
    target.

t.c/2
t.c/2
13
Azimuth (or along-track) Resolution
  • The shorter wavelength (?) and longer antenna (D)
    will improve azimuth resolution.
  • The shorter the wavelength, the poorer the
    atmospheric and vegetation penetration capability
  • There is practical limitation to the antenna
    length, while SAR will solve this problem.

14
SAR
A major advance in radar remote sensing has been
the improvement in azimuth resolution through the
development of synthetic aperture radar (SAR)
systems. Great improvement in azimuth resolution
could be realized if a longer antenna were used.
Engineers have developed procedures to synthesize
a very long antenna electronically. Like a brute
force or real aperture radar, a synthetic
aperture radar also uses a relatively small
antenna (e.g., 1 m) that sends out a relatively
broad beam perpendicular to the aircraft. The
major difference is that a greater number of
additional beams are sent toward the object.
Doppler principles are then used to monitor the
returns from all these additional microwave
pulses to synthesize the azimuth resolution to
become one very narrow beam.
15
Azimuth resolution is constant D/2, it is
independent of the slant range distance, ? , and
the platform altitude. So the same SAR system in
a aircraft and in a spacecraft should have the
same resolution. There is no other remote sensing
system with this capability.
16
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17
Animation of the Doppler Effect
18
Animation of the Doppler Effect
19
Animation of the Doppler Effect
20
Animation of the Doppler Effect
21
Animation of the Doppler Effect
22
Animation of the Doppler Effect
23
Animation of the Doppler Effect
24
Animation of the Doppler Effect
25
At time n3, the shortest distance and area of
zero Doppler shift
26
Speckle noise
  • Using SAR, we can get high spatial resolution in
    the azimuth dimension (direction). But the
    coherently recording returned echoes (SAR) also
    causes speckle noise.
  • For one-single channel SAR system, the speckle
    noise has a multiplicative nature for the
    amplitude and an additive nature for the phase.
  • For multi-dimensional (or polarimetric) SAR (or
    PolSAR) system, speckle noise is even
    complicated.
  • There are two ways to remove speckle noise
  • Using several looks, i.e., averaging takes place,
    usually 4 or 16 looks (N). But lose resolution
    Azimuth resolution N(D/2)
  • Modeling the noise, then remove them.

27
Backscatter
  • The portion of the outgoing radar signal that the
    target redirects directly back towards the radar
    antenna.
  • When a radar system transmits a pulse of energy
    to the ground (A), it scatters off the ground in
    all directions (C). A portion of the scattered
    energy is directed back toward the radar receiver
    (B), and this portion is referred to as
    "backscatter".

28
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29
Amount of backscatter per unit area
http//earth.esa.int/applications/data_util/SARDOC
S/spaceborne/Radar_Courses/Radar_Course_III/parame
ters_affecting.htm
30
Fundamental radar equation
t
31
Frame of the RADARSAT-1 SAR image highlighted
white showing the four regions selected to
compare typical NRCS values of multiyear (blue),
first-year (magenta), marginal ice zone (orange),
and lead (red) ice as observed by Envisat,
RADARSAT, and QuikSCAT on Oct. 12, 2007. The
insert in the top right shows the SIMBA drift
track during Oct. 12, 2007. Superposed are also
the ship positions during the in- and outbound
legs (compare Fig. 1). The total number of
selected 12.5 km x 12.5 km grid cells is 200.
Burcu et al. 2009
32
  • Mean Envisat (diamonds) and RADARSAT-1 (crosses)
    SAR NRCS values obtained for approximated ASPeCt
    observation boxes (see Figure 2) for Oct. 26,
    2007, as a function of ice type (mixtures)
    according to the ASPeCt observations (compare
    Figure 7) grouped from thickest to thinnest ice.
    ASPeCt observations with ice concentration less
    than 80 are not included. The ice type
    (mixtures) are 1 Thick first year, First year
    2 Thick first year, First year, Nilas 3 Thick
    first year, Young grey-white 4 Thick first
    year, Nilas 5 Thin ice types (Young grey,
    Pancake, Nilas, and Grease) ice. Note that
    RADARSAT (0933 UTC), and Envisat (0626 UTC) SAR
    image acquisition times differ by about 3 hours.
    The NRCS values have been separated from each
    other horizontally for better discrimination.
    Error bars annotated to each NRCS value denote
    one standard deviation based on 6400 and 256
    values for RADARSAT (input pixel size 25 m) and
    Envisat (input pixel size 125 m) data,
    respectively. In the top part of the figure
    ASPeCt observations based snow depth is given for
    the primary (triangles) and secondary (squares)
    ice types (right y-axis).


Burcu et al. 2009
33
wrong
Intermediate
34
Penetration ability to forest
Response of A Pine Forest Stand to X-, C- and
L-band Microwave Energy
35
Polarization
  • Unpolarized energy vibrates in all possible
    directions perpendicular to the direction of
    travel.
  • The pulse of electromagnetic energy is filtered
    and sent out by the antenna may be vertically or
    horizontally polarized.
  • The pulse of energy received by the antenna may
    be vertically or horizontally polarized
  • VV, HH like-polarized imagery
  • VH, HV- cross-polarized imagery

36
Penetration ability into subsurface
37
Penetration ability to heavy rainfall
SIR-C/X-SAR Images of a Portion of Rondonia,
Brazil, Obtained on April 10, 1994
38
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39
Radar Shadow
  • Shadows in radar images can enhance the
    geomorphology and texture of the terrain. Shadows
    can also obscure the most important features in a
    radar image, such as the information behind tall
    buildings or land use in deep valleys. If certain
    conditions are met, any feature protruding above
    the local datum can cause the incident pulse of
    microwave energy to reflect all of its energy on
    the foreslope of the object and produce a black
    shadow for the backslope
  • Unlike airphotos, where light may be scattered
    into the shadow area and then recorded on film,
    there is no information within the radar shadow
    area. It is black.
  • Two terrain features (e.g., mountains) with
    identical heights and fore- and backslopes may be
    recorded with entirely different shadows,
    depending upon where they are in the
    across-track. A feature that casts an extensive
    shadow in the far-range might have its backslope
    completely illuminated in the near-range.
  • Radar shadows occur only in the cross-track
    dimension. Therefore, the orientation of shadows
    in a radar image provides information about the
    look direction and the location of the near- and
    far-range

40
Shadows and look direction
Shuttle Imaging Radar (SIR-C) Image of Maui
41
Major Active Radar Systems
  • Seasat, June 1978, 105 days mission, L-HH band,
    25 m resolution
  • SIR-A, Nov. 1981, 2.5 days mission, L-HH band, 40
    m resolution
  • SIR-B, Oct. 1984, 8 days mission, L-HH band,
    about 25 m resolution
  • SIR-C, April and Sept. 1994, 10 days each. X-,
    C-, L- bands multipolarization (HH, VV, HV, VH),
    10-30 m resolution
  • JERS-1, 1992-1998, L-band, 15-30 m resolution
    (Japan)
  • RADARSAT, Jan. 1995-now, C-HH band, 10, 50,
    and 100 m (Canada)
  • ERS-1, 2, July 1991-now, C-VV band, 20-30 m
    (ESA)
  • ASAR on EnviSat, 2002-now, C band
    (ESA)
  • AIRSAR/TOPSAR, 1998-now, C,L,P bands with full
    polarization, 10m
  • NEXRAD, 1988-now, S-band, 1-4 km,
  • TRMM precipitation radar, 1997, Ku-band, 4km,
    vertical 250m (USA and


  • Japan)

42
Active Radar Systems for Mars
  • MARSIS (Mars advanced radar for subsurface and
    ionosphere sounding) of Mras Express, 2003, 1.8-5
    MHz, up to 5 KM deep (ESA)
  • http//sci.esa.int/science-e/www/object/index.cfm
    ?fobjectid34826fbodylongid1601
  • SHARAD (shallow subsurface radar) of MRO, 2005,
    15-25 MHz, up to 1Km deep (ISA-NASA)
  • http//mars.jpl.nasa.gov/mro/mission/sc_instru_sha
    rad.html
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