Remote Sensing Realities | June 2008 Remote Sensing Realities.
BASICS OF REMOTE SENSING
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BASICS OF REMOTE SENSING
Developed ByDr. Mohamed A. Mohamed
With assistance fromMs. Sungmi Park
Pixoneer Geomatics Inc.Phone: (703) 852 2162
E-mail: [email protected]
Summer 2003
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LECTURE 1
Introduction to Remote Sensing
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FROM IMAGE TO INFORMATION
Film
CD-ROM
Ground Reference
The selection tools ordinarily make handedged selections, as if the selections were cut with a razor-sharp knife. Thus,when selections made with these tools are cut or pasted into an image, the individual pixels along the border cna be seen very clearly. This often results in an image that appears unatural. By defining a feather edge around a selection, you can cut and paste the selection without making it stand out dramatically from its surroundings. In this section you will define a feather edge, or border, around a lassoed selection using the Lasso Options dialog box. Note that you can also define a feather edge for rectangular and elliptical marquee selections using the Feather command in the Select menu.
The selection tools ordinarily make handedged selections, as if the selections were cut with a razor-sharp knife. Thus,when selections made with these tools are cut or pasted into an image, the individual pixels along the border cna be seen very clearly. This often results in an image that appears unatural. By defining a feather edge around a selection, you can cut and paste the selection without making it stand out dramatically from its surroundings. In this section you will define a feather edge, or border, around a lassoed selection using the Lasso Options dialog box. Note that you can also define a feather edge for rectangular and elliptical marquee selections using the Feather command in the Select menu.
Photograph
Computer
Energy Source
Data Acquisition
Data Products
andStorage
Image Interpretation
andAnalysis
Productsand
InformationExtraction
Users and
Decision Makers
Maps
Reports
Geographic Information
Systems
Earth Surface Features
ReceiverImage
Tape
Atmosphere
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DEFINITION OF REMOTE SENSING
The science and art of obtaining information about features or phenomena from data acquired by a device that records reflected, emitted, or diffracted electromagnetic energy, and is not in direct contact with the features or phenomena under investigation.
Partially adapted from Lillesand and Keifer, 2000
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HISTORY OF REMOTE SENSING• Born in 1839, photography was first used in topographic
surveying in 1840’s• First aerial photograph was taken from a balloon in 1858• Three-Color photographic process was developed in 1861• Invented in 1903, airplane was first used as a camera
platform in 1909.• Aerial photography was extensively used for reconnaissance
during World War I. • Photo interpretation and photogrammetric mapping
techniques and instruments were greatly developed during World War II
• The lunar missions in 1960’s marked the era of space imaging
• First imaging satellites were launched in early 1970’s
Adapted from Lillesand and Keifer, 2000
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RADIATION PRINCIPLES
•Basic Wave Theory
• Electromagnetic Spectrum• Particle Theory
• Sources of Electromagnetic Energy
• Stephan Boltzmann Law
• Blackbody Radiator
• Wien’s Displacement Law
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ELECTROMAGNETIC WAVE
V = Frequency
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BASIC WAVE THEORY
• Electromagnetic energy travels at the speed of light in a harmonic sinusoidal fashion
• The wavelength () is the distance between two successive Peeks
• Wave frequency (v) is the number of peaks passing a point in space per unit time
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WAVELENGTH AND FREQUENCY
• Wavelength:₋ Distance between two
successive peaks
• Frequency:₋ Number of peaks (crests)
that pass a given point in space per unit time
• Amplitude:₋ Height of peak
Wavelength
1 SecondFrequency
8 cycles
4 cycles
Frequency1 Second
Wavelength
8 cycles
4 cycles
Amplitude
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WAVELENGTH MEASUREMENT UNITS
• Angstrom (Å) = 10-10 m or one 10 billionth of a meter
• Nanometer (nm) = 10-9 m or one billionth of a meter
• Micrometer (µm) = 10-6 m or one millionth of a meter
• Millimeter (mm) = 10-3 m or one thousandth of a meter
• Centimeter (cm) = 10-2 m or one hundredth of a meter
• Decimeter (dm) = 10-1 m or one tenth of a meter
• Meters (m) = 100 m or one meter
• Kilometer (dm) = 103 m or one thousand meter
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FREQUENCY MEASUREMENT UNITS
• Hertz (Hz) =one cycle per second
• Kilohertz (KHz) =1000 cycles per second
• Megahertz (MHz) = 106 Hz or million Hz
• Gigahertz (GHz) = 109 Hz or billion Hz
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BASIC WAVE EQUATION
The longer the wavelength the lower the frequency
v is inversely related to
Where: C = Speed of light = Wavelength v = Wave frequency
C = v
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ELECTROMAGNETIC SPECTRUM
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PARTICLE THEORY
Where: Q = Energy of a photon h= Planck’s constant v = Wave frequency
Electromagnetic radiation is composed of manydiscrete units called photons or quanta
Q = hv
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ENERGY/WAVELENGTH RELATIONSHIP
The longer the wavelength the lower its energy content
The photon energy is inversely related to
From Equation 1 & 2 Q = hC
Q = hv ------ 2C = v ------ 1
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SOURCES OF ELECTROMAGNETIC ENERGY
• The Sun
Examples are terrestrial objects
• All matter at temperature above absolute zero (zero degree K or -273 degree C)
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STEPHAN BOLTZMANN LAW
Total energy increases very rapidly with increase in temperature
Where: M = Total radiant from the surface= Boltzmann constant T = Absolute temperature
M = T4
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BLACKBODY RADIATOR
• A hypothetical ideal radiator that totally absorbs and re-emits all energy incident upon it
• All earth surface features are not ideal radiators
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WIEN’S DISPLACEMENT LAW
Wavelength and temperature are inversely related
Where: m = Wavelength of maximum spectral radiantA= ConstantT = Absolute temperature
m =A/T
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GRAPHICAL REPRESENTATION OF WIEN’S DISPLACEMENT LAW
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LECTURE 2
Energy Interaction with the Atmosphere and Earth Surface Features (Objects)
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ENERGY INTERACTION WITH THE ATMOSPHERE & EARTH FEATURES
Scattered Radiation
Em
itted
Rad
iatio
n
Reflect
ed R
adiation
Absorbed
Radiatio
n
RadiationAbsorbed
Inci
dent
Rad
iatio
n
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REFRACTION
• The bending of light when it passes from one medium to another due to differing densities
Where: c = speed of light in vacuum
• The index of refraction (n) is a measure of the optical density of a substance
n = c / cn
cn = speed of light in a substance
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SCATTERING
• Unpredicted diffusion of radiation by particles in the atmosphere
- Mie scatter
• Three types of scatter:
- Rayleigh scatter
- Non-selective scatter
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RAYLEIGH SCATTER
• Atmospheric molecules and tiny particles are much smaller in diameter than wavelength of the interacting radiation
- Example is a blue sky
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MIE SCATTER
• Atmospheric molecule and particle diameters are equal to the wavelength of the interacting radiation
• Water vapor and dust are major causes
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NON-SELECTIVE SCATTER
• Atmospheric molecule and particle diameters are much larger than the wavelength of the interacting radiation
• Water droplets scatter all visible and near-to-mid infrared wavelengths equally
- Examples are fog and white clouds
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ABSORPTION
• Effective loss of energy to atmospheric constituents
• Most efficient absorbers are:
- Water vapor
- Ozone
- Carbon dioxide
• Absorption band is a range of wavelengths in the electromagnetic spectrum within which radiant energy is absorbed by a substance
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ATMOSPHERIC WINDOWS
Courtesy of NASA Goddard Space Flight Center
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ENERGY INTERACTION WITHEARTH SURFACE FEATURES
Where: EI () = Incident energy ER () = Reflected energy EA () = Absorbed energy ET () = Transmitted energy
Energy incident on an element are reflected,absorbed, and/or transmitted
EI () = ER () +EA () + ET ()
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ENERGY INTERACTION WITHEARTH SURFACE FEATURES
EI () = Incident energy
ET () = Transmitted energyEA () = Absorbed energy
ER () = Reflected energy
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ENERGY REFLECTION BYEARTH SURFACE FEATURES
The geometric manner in which objects reflect energy is a function of surface roughness
ER () = EI () - [EA () + ET ()]
• Specular reflector
• Diffuse (Lambertian) reflector
• In-between (near specular, spread, near diffuse)
- Examples are earth surface features
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SURFACE REFLECTANCE
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IDEAL SPECULAR REFLECTOR
Angle of Incidence
Angle of Reflection
ir
i = rFlat Surface that Manifest Mirror-like Reflection
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LAMBERTIAN SURFACE
Uniform reflectance in all directionsScience & Software
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DIFFUSE REFLECTION
It contains information on the “color” of the reflecting surface
In remote sensing, we are most often interestedin measuring the diffuse reflectance properties
of terrain (earth surface) features
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SPECTRAL REFLECTANCE
Where:
= Spectral reflectance ER () = Reflected energy EI () = Incident energy
• The portion of incident energy that is reflected
= ER () / EI () * 100
• It is often expressed as a percentage
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SPECTRAL REFLECTANCE CURVE
Is a graph of spectral reflectance of an objectas a function of wavelength
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SPECTRAL REFLECTANCE CURVE
Wavelength
% R
efle
ctan
ce
10
20
30
40
50
60
0.5 0.6 0.7 0.8 1.1
Near IRBlue Green Red
MSS 4 MSS 5 MSS 6MSS 7
Dead grass
Dry bare soil
Green grass
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ALBEDO
• % reflection off surfaces at particular wavelengths
BLUE GREEN RED INFRARED
50
40
30
20
10
0
Visible Light
0.4 0.5 0.6 0.7 0.8 0.9Microns
Natural Grass
Artificial TurfP
erc
en
t R
efle
cta
nce
• Artificial turf has a low albedo in the Near Infrared (IR) region
• Healthy natural grass has a high albedo in the Near Infrared (IR) region
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SPECTRAL SIGNATURE CURVE
Is a spectral response measured to assess the typeand/or condition of the feature
Tends to imply an absolute or unique pattern
Main characteristic
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SPECTRAL RESPONSE PATTERN
Is the spectral reflectance or emittance of a terrain feature
• Quantitative but not absolute
• Distinctive but not unique
Main characteristics
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SPATIAL EFFECT
Factors that cause the same type of feature at a given point of time to have different spectral
characteristics at different locations
• Same crop in different fields
Example
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TEMPORAL EFFECT
Factors that change the spectral characteristicsof a feature over time
• Vegetation in different seasons
Example
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IDEAL REMOTE SENSING SYSTEM
• Uniform energy source
• Non-interfering atmosphere
• A super sensor
• Series of unique energy/matter interactions at the earth’s surface
• Multiple data users.
• A real-time data handling system
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REAL REMOTE SENSING SYSTEM
•Variable and non-uniform energy sources
• Interfering atmosphere
• Sensors have limited spectral sensitivity
• Energy/matter interactions at the earth’s surface are not unique
• Concerns and issues about multiple data usage
• Data handling system have limited capabilities
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LECTURE 5
• Electromagnetic Energy Detection with Optical and Thermal Imaging Systems
• Concepts of resolution
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SCANNER SYSTEMS
Build up two-dimensional images of the terrain for a swath beneath the plane using either
across-track (whiskbroom) scanningor
along-track (pushbroom) scanning
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WHISKBROOM SCANNING
• Uses a set of detectors, each of which is designed to have its peak sensitivity at a specific wavelength
• Uses a rotating mirror to scan the terrain along scan lines perpendicular to flight line₋ The scanner repeatedly measure energy on both
sides of the platform
• Successive scan lines (contiguous) compose a two-dimensional image
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WHISKBROOM SCANNING
Scanning Direction
Scanning Mirror Detectors
Flight Direction
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RESOLUTION CELL SIZE
• At Nadir:
• At a Scan Angle of
Where: D = Diameter of resolution cell H’ = Flying height above the terrain IFOV
D = H’
D = (H’ sec
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RESOLUTION CELL SIZE VARIATION
Flight Line
H’
Scan Line
H’ θ = H
’ sec
θ
H’ß
ß
ß
θ
(H’ s
ec θ)
ß
(H’ sec2 θ) ß
Adapted from Lillesand and Keifer, 2000
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SWATH WIDTH
Where: W = Swath width H’ = Flying height above the terrain Half the total field of view
W = 2H’ tan
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INSTANTANEOUS FIELD OF VIEW
• Commonly referred to as IFOV
• IFOV is expressed as the angle within which incident energy is focussed on the detector
• The ground area covered by the IFOV is often expressed as a circle and called resolution cell
• At any instant, the scanner sense the energy within the IFOV
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PUSHBROOM SCANNING
• Uses linear arrays of detectors to scan in The direction perpendicular to flight line
• Linear arrays normally consist of charged-coupled devices (CCDs)
• A single array may contain > 10000 CCD
• Each detector is dedicated to sensing the radiation in a single resolution cell
• All scan lines are viewed by all arrays simultaneously
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PUSHBROOM SCANNING
Scanning
Directi
on
Detectors
Flight Direction
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ADVANTAGES OF PUSHBROOM SCANNING
• Each detector has a longer dwell time, over which to measure energy from the res. Cell₋ Better spatial and radiometric resolution
• Greater geometric integrity because of the fixed relationship among detectors
• CCDs are smaller in size, lighter in weight, and require less power for their operation
• Having no moving parts, a linear array system has higher reliability & longer life
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DISADVANTAGES OF PUSHBROOM SCANNING
• Need to calibrate more detectors
• Current CCDs have a relatively limited range of spectral sensitivity
• Commercially available CCDs are not sensitive to wavelength longer than the Near Infrared
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MULTISPECTRAL SCANNERS
• Sensitive to the region from 0.3 - 14 m
• Bands are relatively broader in range
• Three or more bands
• Different bands may have different spatial resolution
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ATLAS SENSOR
Courtesy of NASA Stennis Space Center
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ATLAS COLOR-IR IMAGE OF ATLANTA
Courtesy of NASA Stennis Space Center
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HYPERSPECTRAL SCANNERS
• Sensitive to the region from 0.3 - 2.5 m
• Bands are very narrow in range
• Many to several hundred bands
• Normally all bands have the same spatial resolution
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AVIRIS SENSOR
Courtesy of NASA Jet Propulsion Laboratory
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FOREST FIRE IN BRAZIL (AVIRIS)
Courtesy of NASA Jet Propulsion Laboratory
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THERMAL SCANNERS
• Sensitive to the region from 3 - 14 m
• Band ranges are variable
• Few to several bands
• Normally all bands have the same spatial resolution
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THERMAL INFRARED SCANNER
RadiationSource
ScanningOptics
Dewar
(liquidnitrogen)
ElectricalSignal
AmplifierTapeTapeRecorderRecorder
Glow Tube
7070mmmmFilmFilm
RecorderRecorder
Lens MotorMotor
OscillatingMirror
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VOLCANOLOGY STUDIES
TIMS image draped over 1:4000 DEM
Courtesy of NASA Ames Research Center
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SPATIAL RESOLUTION
A measure of the smallest angular or linear separation between two objects that can be resolved by the sensor
The smaller the object the higher the resolution
i.e. It is the limit on how small an object can be and still be
“seen” by a sensor as being separate from its surroundings
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SPATIAL RESOLUTION
4 meter x 4 meter 16 meter x 16 meter
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± < 0.2 ± 0.4 ± 61:500 1:1,000 1:2,500 1:25,000
± 5 ± 121:50,000
Standard Error in Position (RMSE meters) SCALE
± 1
Developed Area Regional Area
Urban Rural Undeveloped
Urban - Distr ibution Cross Country Transmission
Facilities Lease Holdings Dev. Area Lease H old Undeveloped
Urban Area & Construction State - M ulti State R egion
Row Crops, Or chard, Small Fields Field Crops, Large Fields
Regional Sys.
Grazing
LAND MANAGEMENTCITY
COUNTY
STATE
INFRASTRUCTUREUTILITIES
TRANSPORTATION
RESOURCE MANAGEMENTAGRICULTURE
MINERALS & PETROL
1:5,000± 2
Map
Usa
ge
1:10,000
IKONOS( 1 ~ 4 m)
IRS/Kompsat( 5 ~ 10 m)
SPOT/Landsat10 ~ 30 m
Typical Users
SPATIAL RESOLUTION & APPLICATIONS
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SPECTRAL RESOLUTION
i.e.The ability to discriminate fine spectral differences
The higher the number of bands the higher the resolution
The number and dimensions of specific wavelength intervals in the electromagnetic spectrum to which a
remote sensing instrument is sensitive.
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SPECTRAL RESOLUTION
Red
Green
Blue
Grey
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RADIOMETRIC RESOLUTION
The sensitivity of a remote sensing detector to differences in signal strength as it records the radiance flux reflected
or emitted from the terrain.
The higher the number of bits,the wider the range of values, and the higher the resolution
i.e.The ability to discriminate very slight energy differences
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RADIOMETRIC RESOLUTION
8 bit (0 ~ 255 ) 11 bit (0 ~ 2047 )
In 2 bit case, target A and target B has brightness value of 1(can not be recognized as different objects in the image). However, in 4 bit case , target A
has value of 3 and target b has value of 2.
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TEMPORAL RESOLUTION
Frequency of data acquisition over the area
Terms implying temporal resolution:• Revisit capability• Global cycle• Global coverage
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CHANGE DETECTION
The ability to measure temporal effectsor
The ability to quantify change over a period of time
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METHODS OF SCANNERS CALIBRATION
• In laboratories
• Fly over natural and/or man-made targets
• On-Board
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CALIBRATION OF SCANNERS
• Spatial resolution
• Radiometric values
• Spectral bands (ranges & co-registration)
• Signal-to-noise ratio
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IMAGERY
Merits:
Recorded by electronic sensors that generate electrical signals that corresponds to
energy variations in the scene
- Improved calibration potential
- Broader spectral range sensitivity
- Electronic transmittal of data
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LECTURE 7
Microwave Remote Sensing
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PASSIVE MICROWAVE SENSORS
• Radiometers or scanners that operate similar to their optical counterparts
• Use antenna to detect naturally emitted microwave energy (atmosphere, surface features, and sub-surface transmittance)
• Characterized by low spatial resolution (large field of view) due to the relatively small magnitude of emitted energy
• The emitted microwave energy is related to the temperature and moisture properties of the object
• Data from such sensors is typical used by:₋ Meteorologists (atmospheric profile, ozone and water
content)₋ Hydrologists (soil moisture content)₋ Oceanographers (mapping sea ice, currents, winds, and pollutants)
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ACTIVE MICROWAVE SENSORS
• Non-Imaging sensors₋ Profiling devices such as altimeters and scatterometers
that take measurements in one linear dimension
• Imaging sensors: ₋ Radar instruments that record two-dimensional images
of surfaces beneath the platforms₋ In general, image acquisition is not affected by
weather (Clouds, Haze, Dust, etc.)₋ Images can be acquired at day and/or night time
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NON-IMAGING SENSORS• Radar Altimeters:
₋ Look straight down at nadir and transmits short microwave pulses to determine distances of targets through measurement of round trip time delays
₋ Often used for determination of aerial platforms’ altitudes, as well as topographic mapping and sea surface height estimation.
• Scatterometers:₋ Used to precisely measure the amount of energy
backscattered from a target, which depends on surface roughness and the incident angle at which the energy contacts the target
₋ Typically used in oceanographic applications for estimation of wind speeds, and identification of materials and characterization of surfaces in land applications.
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PRINCIPLES OF IMAGING RADAR
• Radar is a range or distance measuring device which consists of a transmitter, a receiver, an antenna, and a data processing and recording system
• The transmitter generates short successive pulses of microwave energy at regular intervals which are focused by the antenna into a beam
• The beam obliquely illuminates a surface at a right angle to the direction of the platform
• Targets (objects) reflects the signal back to the receiver (echo or backscatter)
• The location of an object (based on its distance from the radar) is determined by measuring the time delay between transmission of a pulse and reception of the echo backscattered by that object.
• The forward motion of the platform and the continued processing and recording of the backscattered echo builds up a two-dimensional image of the surface
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MICROWAVE BANDS
Letter Code Frequency Range (MHz) Wavelength Range (cm)
P 220 – 390 136 – 77UHF 300 – 1000 100 – 30
L 1000 – 2000 30 – 15S 2000 – 4000 15 – 7.5
C 4000 – 8000 7.5 – 3.75
X 8000 – 12500 3.75 – 2.4Ku 12500 – 18000 2.4 – 1.67K 18000 – 26500 1.67 – 1.18
Ka 26500 – 40000 1.18 – 0.75
Wavelength (λ) in cm = 30000 / frequency in MHz
Adapted from Henderson and Lewis, 1998
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EXAMPLES OF RADAR IMAGERY
L-Band X-Band
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POLARIZATION
Transmission of energy in either a horizontal (H) or vertical (V) plane
Horizontal (H) Vertical (V)
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PARALLEL POLARIZED SYSTEM
Sends and receives signal in same polarization (HH) or (VV)
Horizontal (HH) Vertical (VV)
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CROSS-POLARIZED SYSTEM
• Sends in one polarity and receives in another polarity (VH) or (HV)
• Requires a second antenna
• With a second antenna two images can be recorded simultaneously (HH-HV) or (VV-VH)
• These pairs of images (dual polarization images) can be analyzed for differences
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CROSS-POLARIZED SYSTEM
Vertical Horizontal (VH) Horizontal Vertical (HV)
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POLARITY EFFECT ON IMAGERY
HH Polarization HV Polarization
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MULTI-CHANNEL RADAR
• Records four images simultaneously
• Two polarities and two different wavelengths₋ Band X HH₋ Band X HV₋ Band L HH₋ Band L HV
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SIDE-LOOKING AIRBORNE RADAR (SLAR) VIEWING GEOMETRY
Image SwathImage Swath
Look AngleLook Angle
90˚90˚
90˚90˚
Radar PulseRadar Pulse
Depression AngleDepression Angle
Nadir Line orNadir Line orGround TrackGround Track
Radar BeamRadar Beam
IncidenceIncidenceAngleAngle
Radar GroundRadar GroundContactContact
Ground RangeGround Range
Across TrackAcross Track
Along TrackAlong Track
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RADAR PARAMETERS
• Azimuth direction Direction of flight
• Range (look) direction Direction of illumination which is at right angle to azimuth direction₋ Significantly impact feature interpretation₋ Enhancement or suppression of linear features depends on their
relative orientation to range direction
• Depression angle (γ) Angle between the range direction and the electromagnetic pulse from the radar antenna to a point in the ground
• Incident angle (θ) Angle between the radar pulse and a line perpendicular to the surface it contacts
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RANGE RESOLUTION
• The resolution in the across-track direction which is proportional to the length of the microwave pulse₋ The shorter the pulse length, the finer the resolution
• Range resolution (Rr) = τ.c/2cosγ₋ τ = duration of transmission₋ c = speed of light₋ γ = depression angle
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SLANT RANGE RESOLUTION
AA BB CC DD
All objectsAll objectsdistinguishabledistinguishable
Radar PulseRadar Pulse
AA BB CC DD
Radar PulseRadar Pulse
Cannot distinguishCannot distinguishbetween A & Bbetween A & B
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AZIMUTH RESOLUTION
• Determined by computing the width of the terrain strip illuminated by the radar beam₋ The angular beam width is directly proportional to
the wavelength of the transmitted pulse₋ The beam width is inversely proportional to
antenna length
• Azimuth resolution (Ra) = S x γ / L₋ S = slant range₋ γ = depression angle₋ L = antenna length
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AZIMUTH RESOLUTION
A & B areresolvable C & D are not
resolvable
IlluminatedArea
Antenna
AB
CD
Beam Width
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GEOMETRIC DISTORTION OFRADAR IMAGERY
• Slant-range scale distortion
• Relief displacement₋ Foreshortening₋ Layover
• Shadowing
Inherent geometric distortions in radar imagery are caused by the following:
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SLANT-RANGE SCALE DISTORTION
• Occurs because radar measure distance to objects in slant ranges (not horizontal along the ground distances)
• Objects in the near range are more distorted (compressed) than those in the far range
• Can be easily corrected by using trigonometry to calculate ground-range distances to objects
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RELEIF DISPLACEMENT
• A one-dimensional displacement along the range (look) direction
• Higher Objects are displaced towards the sensor
• Radar foreshortening and layover are typical consequences of relief displacement
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FORESHORTENING OF SLOPE• Occurs when the radar beam reaches the base of a high object
before it reaches the top
• Slopes are compressed. Severity of compression depends on angle of slope in relation to incident angle of radar beam
• Maximum compression occurs when the base and top are imaged simultaneously (radar beam is perpendicular to slope)
BA
A’ B’
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SEVERITY OF FORESHORTENING
Very severe slope compression
Maximum slope compression
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FORESHORTENING OF SLOPES
Courtesy of RADARSAT Corporation
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LAYOVER OF SLOPE
• Occurs when the radar beam reaches the top of a high object before it reaches the base
• Very severe at the near range with small incident angles
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LAYOVER OF SLOPE
Courtesy of RADARSAT Corporation
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RADAR SHADOWS
Radar Image
Photo Image Shadow
• Result from foreshortening and layover
• Occur in the down range direction behind vertical features and steep slopes
• Radar beam does not illuminate the surface
• Shadows appear dark
• Objects in shadows are obscured
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RADAR SHADOWS
Courtesy of RADARSAT Corporation
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RADAR IMAGE INTERPRETATION
• Images are a result of different factors than aerial photos₋ degree of reflectance in one wavelength₋ angle of depression₋ negative terrain: absence of data in the shadows
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TONES ON A RADAR IMAGE
• Measure of backscatter strength
• The stronger the return the brighter the area on the image
• Light tones: prominent cultural and topographic features
• Varying tones: cultivated fields and most terrain surfaces
• Dark tones: calm water bodies, smooth ice, and some depositional landforms
• Uniform tones: relatively homogeneous feature
• Grainy or speckled tones: rough surfaces
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SUPERIOR, WISCONSIN
StorageTanks
City
Water
Sandy Deposits
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ALBERTA, CANADA
Road
Lakes
SelectiveClearcut
Drumlins
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DETRMINING FLIGHT DIRECTION
• What direction was the aircraft flying if the SLAR was mounted on the port (left) side?
A
BC D
Choices…
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FEATURES IDENTIFICATION
PowerLines
ErodedAnticlines
CultivatedFields
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