intro rs-i
TRANSCRIPT
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FUNDAMANTALS OF REMOTE
SENSING
R.S.DWIVEDI
PART-I
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Remote sensing is the measurement or
acquisition of some property of an object or
phenomenon, by recording device that is not in
physical or intimate contact with the object or
phenomenon under study (Colwell, 1983).
WHAT IS REMOTE SENSING?
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SCOPE
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COMPONENTS OF A SATELLITE REMOTE
SENSING SYSTEM
-Launch Vehicle
-Platform (Satellite)
-Sensor- Data Reception
-Data Processing
-Interpretation/Analysis
-Generation of thematic maps / area statistics/ reports
-Development of Decision Support System (DSS)-Creation of digital database
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DATAArchive
Concept of Remote SensingFrom Space Data to information
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TYPES OF SENSORS
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ACTIVE SENSORS Own energy source for
illumination
Emits radiation which isdirected toward the target tobe investigated
Microwave
Optical
PassiveActiveActive
Passive
LIDAR(ALTM)
Visible, Near &Thermal Infrared ImagersImaging Spectrometer
IMAGINGRADARS
Multi FreqMicrowaveRadiometers.Imagingpossible withscan optionAtmosphericSounders
NON-IMAGINGScatterometerAltimeterRain MappingRadar
PASSIVE SENSORS
Energy from Sun Reflected, Absorbed &
Re Emitted as Thermal IRDuring day for reflected wavelengths
Emitted Energy (such as thermal
infrared) can be detected day or night
SENSORS
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SIDE LOOKING RADARSYSTEMS
IMAGING NONIMAGING
SLR
RAR
SAR
Active
SPACE BORNE SAR
AIR BORNE SAR
GROUND BASED SAR
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REMOTE SENSING : HISTORICAL
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LAUNCH VEHICLE
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Launch Vehicle Family
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WAVE MODELEMR has been thought of as electromagnetic wave that travels through
space at a speed of light (Maxwell 1831).
It consists of two fluctuating fields one electric and the other magnetic.
The two vectors are at right angles (orthogonal) to one another, and both are
perpendicular to direction of travel.
EMR is generated whenever an electrical charge is accelerated.
The wavelength () of the EMR depends upon the length of time that the
charged particle is accelerated. Its frequency (v) depends on the number of
accelerations per second.
Electromagnetic Radiation
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Electromagnetic Spectrum
Violet: 0.4 - 0.446 mm
Blue: 0.446 - 0.500 mm
Green: 0.500 - 0.578 mm
Yellow: 0.578 - 0.592 mm
Orange: 0.592 - 0.620 mm
Red: 0.620 - 0.7 mm
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Optical Infrared (OIR) Region
Visible 0.4-0.7mm
Near infrared (NIR) 0.7-1.5 mm
Shortwave infrared (SWIR) 1.5-3.0 mmMid-wave infrared (MWIR) 3.0-8.0 mm
Thermal infrared (TIR) 8.0-15 mm
Far infrared (FIR) Beyond15 mm
Microwave Region
P Band 0.3 - 1GHz (30 -100 cm)
L Band 1 -2 GHz (15 - 30 cm)
S Band 2 - 4 GHz (7.5 - 15 cm)
C Band 4 - 8 GHz (3.8 - 7.5 cm)
X Band 8 - 12.5 GHz (2.4 - 3.8 cm)
Ku Band 12.5 - 18 GHz (1.7 - 2.4 cm)
K Band 18 - 26.5 GHz (1.1 - 1.7 cm)
Ka Band 26.5 - 40 GHz (0.75 - 1.1 cm)
1 GHz = 109 Hz
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Electromagnetic Radiation
c
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Wavelength and frequency
c = where c = 3 x 108 ms-1
in vacuum
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The particle theory suggests that electromagnetic radiation is
composed of many discrete packets of energy called
Photons or Quanta.
The energy of each quantum is given by
Q = h
where Q is energy of quantum (J), h is Plancks constant (6.626
x 10-34 J-s) and is frequency
Also, Q = hc/ implies the longer the wavelength involved, the lower
its energy content.
Electromagnetic RadiationParticle Theory
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RADIATION LAWS
An ideal thermal emitter is called a
Blackbody. Also known as Planckian
radiator.
That is, its emissivity is equal to 1. In otherwords it radiates the entire energy whatever
it absorbed.
Black Body
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Gray Body
A gray body is one for which emissivity
value is constant but less than unity.
A selective radiator is one for which
emissivity value varies with wavelength..
RADIATION LAWS
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Radiant exitances for a blackbody, gray body anda selective radiator
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PLANCKS LAWPlancks Law: The most general law
Planck's Law allows us to calculate total energy radiated in
all directions from a blackbody (radiator) for a particular
temperature and wavelength.
M( )= C1 -5/[exp(C2/ T) - 1]
where
C1(2 hc2) = 3.74 x 10-16 W m-2,
C2 (hc/k)= 1.44 x 10-2 m K,
wavelength ( m),
T temperature ( K),
M( spectral exitance (W m-2 m-1),
k = 1.38 x 10-23 W s K-1, h = 6.625 x 10-34 J s
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Weins Displacement Law
The dominant wavelength, or wavelength at which a blackbodyradiation curve reaches a maximum, is related to its
temperature
m = (k/T)
where m is wavelength of maximum spectral radiant exitance( m), k = 2898 m K, T is absolute temperature in K
Rayleigh-Jeans law
This law explains blackbody emission at higher wavelengths:
M()=C1-4T/C2
BLACK BODY RADIATION
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RADIATION LAWS
Spectral distribution of
energy radiated by
blackbodies at various
temperatures9.6 m