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Introduction to Optical/Thermal Remote Sensing

J. A. Sobrino, J. C. Jiménez-Muñoz

(University of Valencia, Spain)

sobrino@uv.es, jcjm@uv.es

OUTLINE

Basic radiometric magnitudes

Basic laws of radiation

Radiative transfer equation

Optical remote sensing: reflectivity

Thermal remote sensing: thermal properties

Atmospheric correction: solar & thermal

Measurements

Spectral regions

Spectral range (mm) Term

0.4-0.7 Visible (VIS)

0.7-1.5 Near Infrared (NIR)

1.5-2.5 Short-Wave Infrared (SWIR)

3-5 Mid-Infrared (MIR)

8-14 Thermal Infrared (TIR)

VIS, NIR, SWIR: dominated by reflected solar energy TIR: dominated by surface emission MIR: reflected solar energy + surface emission

RADIOMETRIC MAGNITUDES

Radiative field: EM field of the wave propaging between the source and the

detector.

Energy of the EM wave Radiant energy: Q [J]

Radiant energy/time: Radiant flux f = dQ/dt [W] (W=J·s)

(f: flux of the Poynting vector)

f Does not provide information about distribution/direction of radiation

Basic magnitudes

Conservation of energy

fi = ft + fr + fa

i: incident

t:transmitedo

r:reflected

a:absorbed

Radiant flux density: F=df/dS [Wm-2] (f through an element dS)

Irradiance (E): F when the surface receives the radiation

Emittance (M): F when radiation is emitted by a source

F does not include information about direction

Radiant intensity I = df/dW [Wsr-1] : radiante flux in a given dW

I : used to characterize emission from point sources

Basic magnitudes

Radiance

Radiant flux (f) in a given dW through a

perpendicular surface (dScosq) to the

propagation direction.

22 1d dI

L [Wm sr ]d dScos dScos

f

q q

W

Basic magnitudes

2

dAd Esfera : 4 [sr]

r

Fuente puntual isotropa : I4

Superficie Lambertiana :

L( ) L(0º ) I( ) I(0º )cos (Ley coseno)

Radiancia / Emi tancia :

M L( , )d cos L( , )cos sen d d

Superficie Lambertiana : M L

f

q q q

q f q q f q q q f

W W

W

Sphere

Isotropic point source

Lambertian surface:

(cosine law)

Radiance/Emittance

Lambertian surface:

Spectral magnitudes

The interaction mechanisms are dependent on l

The previous magnitudes are spectral magnitudes!!!

(Ql, fl, Il, El, etc)

2ll m

dL WL

d m sr mSpectral radiance:

(In practice spectral magnitudes are measured over a certain band witdh)

MAGNITUDE SYMBOL DEFINITION UNITS

Radiant energy Q - J

Radiant flux f dQ/dt W

Emittance M df/dS W m-2

Irradiance E df/dS W m-2

Radiant intensity I df/dW W sr-1

Radiance L d2f/(dWdScosq) W m-2 sr-1

Spectral radiance Ll dL/dl W m-2 sr-1 mm-1

Summary of radiometric magnitudes

REFLECTIVITY:

Ratio between reflected and incident fluxes = fr/fi

ABSORTIVITY: Ratio between absorbed and incident fluxes

= fa/fi

TRANSMISIVITY: Ratio between transmitted and incident fluxes

t = ft/fi

EMISSIVITY Ratio between the emittance of a body and the emittance of a blackbody at the same temperature = M/Mn

Adimensional magnitudes

Conservation of energy

fi = ft + fr + fa + + t = 1

Spectral magnitudes

l, l, tl, l

Basic laws of radiation

Planck law

Planck (1900) found a mathematical description for the spectra distribution of the radiance emitted by a blackbody:

k: Stefan-Boltzmann constant (1.38·10-23 J K-1)

c: speed of light (2.9979·108 m s-1)

T: absolute temperature (K)

c1 , c2 : radiation constants

c1 = 2hc2 = 1.19104·108 W mm4 m-2 sr-1 ; c2 = hc/k = 14387.7·104 mm K

(l in mm, then Planck’s function in W m-2 mm-1 sr-1)

5

1

2

( )

exp 1

cB T

c

T

l

l

l

3 22( )

exp 1

h cB T

h

kT

2

cc d dl l

l

ll

l

1kT

hcexp

hc2M

5

2

,n

Blackbody is lambertian

M(T) = L(T)

Earth: 300 K

Sun: 6000 K

Planck’s law is fundamental in thermal remote

sensing. It related emitted radiance with body

temperature from the measured radiance in a

given sensor bands, we can obtain the radiant

temperature

2

15

cT

cln 1

Bl

ll

Stefan-Boltzmann law

Example: emittance for 300 K

(Earth) and 6000 K (Sun).

The figure includes the bands of

the NOAA/AVHRR sensor.

48 2 4

4

TL(T) L (T)d ( 5.67·10 Wm K )

M(T) T

l

l

l

Total emissive power of a blackbody (no consideration of the spectral distribution) is

a function of T4

Stefan-Boltzmann constant ()

Wien’s displacement law

For an object at a constant kinetic temperature, the radiant energy (flux) varies as a function of wavelength (see Planck’s law).

The radiant energy peak (lmax) is the wavelength at which the maximum amount of energy is radiated.

As temperature increases, the radiant energy peak shifts to shorter wavelengths. This shift is described by Wien’s displacement law:

max

3

max

dB(T)0 T 2.8975·10 m·K

d l l

ll

max 6 3 1 5

5

B4.7961·10 (Wm sr K )

T

l

When l=lmax:

Wien’s displacement law

Sun (6000 K): lmax=0.5 mm (VIS) Earth (300 K): lmax=9.7 mm (TIR)

Radiation laws need to be corrected for the emissivity, since real materials are not perfect blackbodies:

B(T) B(T)

Approximations (Planck’s law)

2 2 2c c c1 ( cortas) T 5000 m·K exp 1 exp

T T Tl l m

l l l

Wien’s radiation law

52 2 2c c c1 ( largas) T 10 m·K exp 1

T T Tl l m

l l l

Rayleigh-Jeans’ law

(In this case, blackbody radiance and temperature show a linear relationship)

Examples:

5 m WienT 1000K

100 m R J

16.6 m WienT 300K

333.3 m R J

l m

l m

l m

l m

Kirchhoff’s law

When a radiation source is surrounded by other radiation sources, it emits

radiation but also absorbs radiation.

The temperature will depend on the balance between emitted and absorbed

energy.

Radiation equilibrium: emitted energy = absorbed energy (all l)

absorbida emitidaL B (T) L B (T)l l l l l l l l

Kirchhoff’s law: for a given l, the absorptivity of the surface equals

the emissivity of the surface, at the same temperature.

Superficies opacas ( 0) 1l l lt Opaque surfaces

Fundamental approach in

radiometry, since emissivity

values can be obtained from

reflectivity measurements

Radiative transfer

It describes the processes involved in the propagation of the radiation from

the surface to the sensor (or sun-to-sensor) through the atmosphere

RADIATIVE TRANSFER EQUATION (RTE)

RTE allows to perform atmospheric corrections and also

forward simulations

“CLASSIC” THEORY OF RADIATIVE TRANSFER:

RTE is obtained from an energy balance (conservation of energy)

(Chandrasekhar, 1960; Lenoble, 1993)

“MODERN” THEORY OF RADIATIVE TRANSFER:

RTE obtaiend from wave theory (Maxwell Eqs. + statistical considerations)

(Apresyan y Kravtsov, 1996).

Radiative Processes

a

s

a s e

dLL

dn

dLL

dn

dLL L

dn

e

sc em

dLL J

dn

J J J

L

L+dL

dn

absorption

scattering

abs+scat

abs+scat+sources

Source function

n

(Spectral magnitudes)

dL = -a L dx L(x2) = L(x1) exp(-da)

2

1

( )x

a ax

x dxd

)exp()(

)(

1

2a

xL

xLdt

)(

)(lnln

2

1

xL

xLa td

t

1)(

)()(

1

21

xL

xLxL

Absorption

Path between x1 and x2

Beer-Lambert-Bouguer law

Volumetric

absorption coefficient (m-1) Optical depth (absorption)

Homogeneous media: a·Dx

Transmissivity

da

Absorptivity (with reflexion: + + t = 1)

dL = -s L dx 2

1

( )d x

s sx

x dx

Scattering (similar to absorption, more complex because of the scattering function)

Let us to consider a volume element dv. The incident ray is characterized by its irradiance E over dv. The scattered radiant flux by dv in a given direction n and angle q inside a solid angle dW is given by

d2f = f(q) E dv dW f(q) (m-1sr-1): scattering function (characterizes the angular distribution of scattered photons)

Total flux lost in the scattering (integration over all the space):

Wespacio

dfEdvd )(qf

For a given volume (dV (dv = dS dx), the incident flux is given by f = E dS

df = -s f dx = -s E dv Wespacio

s df )(q

)(4

)( q

q fp

s

q 4)( Wespaciodp

mmqqq0

1

12)()( dpdsenp

Normalized phase

function

;

General case: Absorption + Scattering

e = a + s d = da + ds

e

s

s e

a e1

Similar to the previous cases

Extinction coefficient (e) and Total optical depth (d)

Single-scattering albedo

(ratio between absorption and scattering processes)

Conservative case: single-scat. albedo = 1 No loss of radiative energy

(no absorption)

Radiative Transfer Equation

“CLASSIC” THEORY OF RADIATIVE TRANSFER:

-Phenomenological considerations

-Based on the conservation of energy

-Radiance is an energetic variable. Energy balance:

Variation

of L(R,n)

along the

direction n

Loss of energetic flux

because of absorption

and scattering from

direction n to direction

n’

Increase of energy

flux in the direction n

because of scattering

from other directions

n’

Increase in the

flux because of

the sources

= - + +

dn

d

dV=ddn

Ll(R,n)ddW [Ll(R,n)+dLl(R,n)]ddW f1

f2

-el(R)Ll(R,n)dnddW

f3

el(R)Jl (R)dndd

dW

n

dW

f4

e

( , )= - ( ) ( , ) ( , )l

l l l dL

L Jdn

R nR R n R n

Radiative Balance

R.T.E.

OPTICAL REMOTE SENSING

REFLECTIVITY

Definitions of reflectivity

a) lambertian (perfectly diffuse) b) non-lambertian (directional or diffuse) c) Specular d) Hot spot

r

i

d

d

f

f Adimensional magnitude. Ratio between reflected

and incident fluxes

Hemispherical reflectance rh

=df

h

dfi

d2f = LdWdScosq

dW =dA

r2=

rsenq (rdq )dj

r2

ü

ýï

þïÞ df

h= dj

0

2p

ò LdScosqsenq dq0

p

dfi= EdSÞ r

hq ,j( ) =

1

Edj

0

2p

ò LdScosqsenq dq0

p

Para una superficie lambertiana :

dfh

= LdS dj0

2p

ò cosqsenq dq0

p

2ò = pLdS Þ rh

=pL

E=

M

E

Reflectividad hemisferica espectral : rh,l

=M

l

El

(Ratio between emittance and irradiance)

Lambertian surface

BIDIRECTIONAL REFLECTANCE DISTRIBUTION FACTOR: BRDF NATURAL SURFACES ARE NOT LAMBERTIAN distribution of radiance shows a significant angular dependence

r i i r r i r i i r r i 1

r i i r r

i i i i i i i i

dL , , , ,E dL , , , ,Ef , , , sr

dE ( , ) L ( , )cos d

q f q f q f q fq f q f

q f q f q

Nicodemus et al. (1977):

r i

i

ri i r r i

i

r i i r r i i i i r

i i i i

d( , ; , ;L )

d

f ( , ; , )L ( , )d d

L ( , )d

f q f q f

f

q f q f q f

q f

W W

W

Definition of reflectivity from BRDF:

r

r,id

dBRF

d

f

f

Bidirectional Reflectance Factor (BRF):

Ratio between reflected flux and reflected flux of a perfectly diffuse (ideal) surface

Different definitions of reflectivity (Sobrino, 2000)

Reflectivity of natural surfaces Soils

Reflectivity increases with increasing wavelength Depends on: -texture -water content -organic matter -iron oxides -roughness

Reflectivity of natural surfaces Water and Snow

Water: low reflectivity Depends on: -depth -chlorophyll, nutrients… -roughness Snow: high reflectivity l<0.8 mm, low reflectivity l>1.5 mm Decreases with the snow age Fresh snow > frozen snow

Reflectivity of natural surfaces Green Vegetation (Leaves)

THERMAL REMOTE SENSING

Thermal properties & Emissivity

Thermal Remote Sensing

Less attention has been given (in comparison to VNIR-SWIR data exploitation)

Necessary for a better understanding of land surface processes and land-atmosphere interactions (most of the fluxes at the surface/atmosphere interface can only be parameterized through the use of TIR data).

Key parameters:

LAND SURFACE TEMPERATURE (LST)

LAND SURFACE EMISSIVITY (LSE, ) – spectral magnitude!

Low Resolution:

LST: climatology, land cover change, SST

LSE: not exploited. Used as input to LST algorithms.

High Resolution:

LST: energy balance (heat fluxes => ET => water management)

LSE: geology (mineral mapping), identification of characteristic feautres in the spectrum… and also land cover change

Thermal Remote Sensing

Heat energy is transferred from one place to another by 3 means: Conduction, Convection and Radiation Materials at the surface of the earth receive thermal energy primarily in the form of radiation from the sun. All matter radiates energy at thermal IR wavelengths (around 3 to 15 mm) both day and night (VNIR data only available at day!). Kinetic heat: energy of particles of matter in a random motion, which causes particles to collide, resulting in changes of energy state and the emission of electromagnetic radiation form the surface of materials (radiant energy). Kinetic temperature: concentration of kinetic heat of a material. Measured with a thermometer (direct contact). Radiant temperature: concentration of radiant flux of a body. Measured remotely by radiometers.

Reflectivity, absorptivity, transmissivity

Radiante energy striking the surface of a material is partly reflected, partly absorbed, and partly transmitted (conservation of energy)

reflectivity + absorptivity + transmissivity=1 Spectral magnitudes determined by properties of matter Opaque materials: reflectivity + absorptivity = 1

Blackbody. Emissivity.

The concept of blackbody is fundamental to understanding heat radiation.

Blackbody: theoretical material that absorbs all the radiant energy that strikes it (absorptivity=1). It also radiates all of its energy in a wavelength distribution pattern that is dependent only on the kinetic temperature.

A blackbody is a physical abstraction: no material has an absorptivity of 1 and no material radiates the full amount of energy.

Real materials: a property called emissivity is introduced, defined as the ratio bewteen the real radiant flux and the radiant flux from a blackbody. It is a spectral magnitude.

Blackbody: emissivity=1. Real material: emissivity<1.

Effect of emissivity on measured radiant temperature: “Real” temperature: 10 ºC Radiometer 1: Emis=0.06. T= -133 ºC Radiometer 2: Emis=0.97. T=8 ºC The difference for the radiometer 1 is more than 140 ºC!!! The difference for the radiometer 2 is only 2 ºC becuase emissivity is near to 1 (blackbody).

RADIOMETER 1 RADIOMETER 2

Other thermal properties

Thermal conductivity: rate at which heat will pass through a material. Rocks and soils are relatively poor conductors of heat.

Thermal capacity: ability of a material to store heat. Water has a high value of thermal capacity.

Thermal inertia: measure of the thermal response of a material to temperature changes. It depends on thermal conductivity, density and thermal capacity. Materials with a high thermal inertia (sandstone, basalt) strongly resist temperature changes and have low DT (maximum-minimum T in the daily cycle).

Apparent Thermal Inertia: it can be measured from remote sensing methods, and depends on DT and albedo (measurements of thermal inertia require contact methods).

Thermal diffusivity: rate at which temperature changes within a substance.

Emissivity spectra of natural surfaces

Surface emissivity is a key variable in thermal remote sensing. Accurate retrievals of LST from remote sensing techniques rely on accurate estimations of surface emissivity.

Natural (and manmade) surfaces are not perfect blackbodies. The emissivity spectra needs to be characterized.

Spectral libraries include several emissivity spectra measured in the laboratory for different surfaces. These spectra are useful for simulation purposes.

MODIS Emissivity Library

http://www.icess.ucsb.edu/modis/EMIS/html/em.html

ASTER Spectral Library

http://speclib.jpl.nasa.gov/

Natural surfaces: Rocks

0.80

0.82

0.84

0.86

0.88

0.90

0.92

0.94

0.96

0.98

1.00

7 8 9 10 11 12 13 14 15

longitud de onda (mm)

em

isiv

idad

basalto

diorita

cuarzo

mármol

0.80

0.82

0.84

0.86

0.88

0.90

0.92

0.94

0.96

0.98

1.00

7 8 9 10 11 12 13 14 15

longitud de onda (mm)

em

isiv

idad

Agua

hierba seca

hierba verde

Natural surfaces: Water and Vegetation

Spectral features

A sample and the medium in which it is embedded for the purpose of taking and infrared spectrum will always having differing dispersions, although their indices of refraction may match at a center frequency of interest. In general, there will therefore be a wavelength at which the sample+medium have a maximum transparency. Christiansen frequency: the frequency of maximum transparency.

Reststrhalen bands: reflectance phenomenon in which EM radiation within a narrow energy cannot propagate within a given medium due to a change in refractive index concurrent with the specific absorbance band of the medium. Normally-inciden Reststrahlen band radiation experiences strong-reflection or total-reflection from that medium.

Reststrahlen bands manifest as a minima in emissivity.

quartz corn

“a” shows a strong minimum at 9,67 mm, related to the Reststrhalen bands Christiansen bands for quartz

0

10

20

30

40

50

60

70

80

90

100

0.0 0.5 1.0 1.5 2.0 2.5

longitud de ona (mm)

refl

ecti

vid

ad

(%

)

0

10

20

30

40

50

60

70

80

90

100

0.0 0.5 1.0 1.5 2.0 2.5

longitud de onda (mm)

reflecti

vid

ad

(%

)

REFLECTIVITY (VNIR) vs

EMISIVITY (TIR)

Green vegetation

Rock (quartz)

Emissivity/Temperature

What happens if measurements are not corrected for emissivity?

T 1

T 5

D D

T 300K T 60

1% T 0.6K

D D

D D

Sample (8-14 mm) DT (=1)

Sand 0.8-0.9 15-6

Clay 0.94-0.98 4-1

Water, Vegetation 0.97-0.99 2-0.6

Snow 0.99 0.6

(T=300K)

0.84

0.86

0.88

0.90

0.92

0.94

0.96

0.98

1.00

6 7 8 9 10 11 12 13 14 15 16

Longitud de Onda (m)

Em

isiv

idad

Coníferas

Mármol

6.0

6.5

7.0

7.5

8.0

8.5

9.0

9.5

10.0

10.5

6 7 8 9 10 11 12 13 14 15 16

Longitud de Onda (m)

Rad

ian

cia

(W

m-2

sr-1

m

-1)

B(Ts)

e1*B(Ts)

e2*B(Ts)

288

290

292

294

296

298

300

302

6 7 8 9 10 11 12 13 14 15 16

Longitud de Onda (m)

Tem

pera

tura

(K

)

Ts

Ts1

Ts2

Emissivity correction Surfaces are not blackbodies: ≠1 y =f(l) Some natural surfaces behave as black/grey-bodies (e.g. water, vegetation)

Emissivity spectra

Radiant energy (radiance)

Temperature

Atmospheric Correction

SURFACE

ATMOSPHERE

The atmosphere mainly absorbs the thermal radiation emitted by the surface, and also scatter in the VNIR (solar) range. This loss of radiation needs to be compensated to recover the at-surface signal (Atmospheric Correction).

LlTOA = Ll

SUN tl lsur + Ll

path

LTOA: At-sensor registered radiance (TOA, Top Of Atmosphere). LSOL: Extraterrestrial solar irradiance (corrected for excentricity and zenithal solar angle). t: Total atmospheric transmissivity: Sun-to-target (t), target-to-sensor (t) t = t·t . sur: at-surface reflectivity. Lpath: path radiance.

Lpath

LSun

tLSun sur(tLSun)

t[sur(tLSun)]

ATMOSPHERIC CORRECTION IN THE SOLAR RANGE: SIMPLIFIED APPROACH

0,2

cosSOL zL Ed

l l

q

At-surface reflectance is obtained after compensation of path radiance and atmospheric transmissivity

ll

lll

t

SOL

ocaTOA

L

LL minsup

In terms of reflectivity the R.T.E. can be expressed as:

lTOA = tl l

sur + lpath

Atmospheric effect

ATMOSPHERIC CORRECTION FROM A SIMPLIFIED APPROACH OF THE R.T.E.

0.0

0.1

0.2

0.3

0.4

0.5

0.6

0.7

0.8

0.9

1.0

7 8 9 10 11 12 13 14 15

longitud de onda (mm)

tra

ns

mis

ivid

ad

LMV

LMI

SAV

SAI

TRO

ATMOSPHERIC CORRECTION IN THE THERMAL INFRARED

O3

8-9.4 mm 10-12.5 mm Atmospheric Windows in the TIR

Tran

smis

sivi

ty

Wavelength (mm)

THERMAL INFRARED - TIR (8-14 mm)

( ) (1 )sen atm atm

sL B T L Ll l l l l l l t

B: Planck’s law

Brightness temperature: LsenB(Tsen)

LST: Ts (l → i)

Physical basis: classical radiative transfer

( ) (1 )sen atm atm

sL B T L Ll l l l l l l t

sup ( ) (1 )erficie atm

sL B T Ll l l l l

supsen atmL L Ll l l lt

supsen atmL L

L l ll

lt

Atmospheric Correction (TIR)

Atmospheric Correction:

The signal measured by the

sensor is not the radiance

coming from the surface

because of the perturbation

of the atmosphere

LST retrievals from remote sensing data require an atmospheric correction and

also a previous estimation of the surface emissivity (we need to solve the coupling

between LST & )

Rigorous algorithms are based in the Radiative Transfer Equation. Algorithms

depend mainly on the spectral characteristics of the TIR sensor

METHODS FOR LST RETRIEVAL:

1 BAND: Single-channel (mono-window)

2 BANDS: Two-channel or split-window

1 BANDS and 2 VIEW ANGLES: Bi-angular (dual-angle)

3 BANDS (multispectral): TES algorithm

Other Methods: TISI, day/night combinations, tri-channel, etc…

LST RETRIEVAL

LST: TWO-CHANNEL ALGORITHMS (2 BANDS)

Based on the “differential absorption” concept, also known as “split-

window”

Differential absorption Atmospheric correction (Ti – Tj)

LST = Ti + c1 (Ti-Tj) + c2 (Ti-Tj)2 + c0 + (c3+c4W)(1-) + (c5+c6W)D

= 0.5 (i - j)

D = i – j

Ti,Tj in K

W in g/cm2

Mathematical structure of the algorithm (Sobrino et al. 1996; Sobrino & Raissouni, 2000)

DUAL-ANGLE ALGORITHMS

Same as split-window, but using two different view angles:

Ti Tn (nadir) Tj Tf (forward)

Emissivities are obtained from VNIR data, and not from TIR data! This avoids the

undetermined problem.

Simplified approach

Emissivity as an average of soil and vegetation emissivities according to the Fractional

Vegeetation Cover (FVC).

NDVI Thresholds Method (Sobrino & Raissouni, IJRS, 2000)

Pixels are classified into bare pixels, mixed pixels and fully-vegetated pixels. Cavity effect is

estimated from a geometric model.

, ,(1 )s vFVC FVCl l l

, ,(1 )

0.985 0.005

red

s v

a b NDVI NDVIs

FVC FVC C NDVIs NDVI NDVIv

NDVIv

l l

l l l l

(1 ) '(1 )i si vi vC F P 2

' 1 1H H

FS S

2NDVI NDVIs

FVCNDVIv NDVIs

EMISSIVITY: SINERGY BETWEEN VNIR & TIR

MEASUREMENTS

REFLECTANCE MEASUREMENTS

(GER, ASD, etc.)

REFERENCE WHITE PANEL: Spectralon, highly reflectant and diffuse (hemispherical reflectance > 99%)

THERMAL RADIOMETERS

CALIBRATION SOURCES DIFFUSE PLATE

BOX FOR EMISSIVITY MEASUREMENTS THERMAL CAMERAS

GONIOMETER

Broadband radiometers (8-14 mm)

RAYTEK ST8

-30 to 100 ºC

0.5 ºC

FOV: 8º

RAYTEK MID

-40 to 600 ºC

0.5 ºC

FOV: 20º

EVEREST 3000

-40 to 100 ºC

0.5 ºC

FOV: 4º

Apogee

IR-120 (Campbell)

-25 to 60 ºC

0.2 ºC

FOV: 20º

multiband:

CIMEL

0.0

0.1

0.2

0.3

0.4

0.5

0.6

7 8 9 10 11 12 13 14 15

longitud de onda (mm)

filt

ro

banda 1: 8-14 um

banda 2: 11.5-12.5 um

banda 3: 10.5-11.5 um

banda 4: 8.2-9.2 um

0.0

0.1

0.2

0.3

0.4

0.5

0.6

7 8 9 10 11 12 13 14 15

longitud de onda (mm)

filt

ro

banda 1: 8-13 um

banda 2: 11-11.7 um

banda 3: 10.3-11 um

banda 4: 8.9-9.3 um

banda 5: 8.5-8.9 um

banda 6: 8.1-8.5 um

MODEL BANDS RANGE ACCURACY FOV

CIMEL 312-1

8-13 mm

8.2-9.2 mm

10.3-11.3

mm

11.5-12.5

mm

-80 a 60 ºC 0.1 ºC 10º

CIMEL 312-2

8-13 mm

11-11.7 mm

10.3-11 mm

8.9-9.3 mm

8.5-8.9 mm

8.1-8.5 mm

-80 a 60 ºC 0.1 ºC 10º

The box method: emissivity measurements

(Buettner y Kern, 1965; Dana, 1969; Sobrino y Caselles, 1989; Nerry et al. 1990)

The box method was designed to measure the surface emissivity. It removes the surrounding (or sky) irradiance using a closed lambertian box. It can be used both at the field (outdoors) or in the laboratory (indoors).

The box method Formulation

SENSOR

LID

2 LIDS

FINAL EXPRESION (T removed!)

1

1

2

1

t ss

t s

L L

L L

1

1

2

1

( ) ( )

( ) ( )

b b

t ss b b

t s

T T

T T

Ideal case: t1: blackbody (=1 y =0) t2: perfect reflector (=1 y =0)

Radiance/Temperature approach: (Slater, 1980): L=aTb

Accuracy of the box method

The box is not perfect, so a correction factor is added:

s 0 d d: depends on the box geometry, temperature and emissivity of the lids

RADIOMETRIA PASIVA

1.-MÉTODO DE LA RADIANCIA ATMOSFÉRICA

Utiliza una superficie reflectante cerrada y lambertiana (Caja)3 medidas para obtener la emisividad

1) Radiometro observa muestra a traves orificio practicado en lacaja

LBBcaja =s B(Ts) + (1-s) B(Ts) = B(Ts)

Supone emisividad caja=0

2) Medida muestra sin caja

LBB=s B(Ts) + (1-s) La

3) Medida de la Radiancia de los alrededores, La

La temperatura del suelo no debe cambiar durante el proceso demedida

Combinando 1) y 2) LBB=s (LBBcaja-La)+ La

sl= LBB-La

LBBcaja-La

Método adecuado cuando alrededor=atmosfera

IT IS ALSO POSSIBLE TO MEASURE THE EMISSIVITY WITH A LAMBERTIAN BOX WITH ONLY 1 “COLD” LID

BOX WITH THE COLD LID

BOX WITHOUT THE LID

FINAL EXPRESSION

RECOMMENDATIONS FOR IN-SITU MEASUREMENTS USING THE BOX METHOD 1 LID: clear-sky, or totally cloudy 2 LIDS: T for the “hot” lid should be higher than the sample T Buettner & Kern (1965): hot water flows Nerry (1988): Electrical resistances Sobrino (1989): Heating by sunlight

Measurements should be performed around midday. Our experience shows a reproductibility better than 1% for temperature differences between the lids of aroudn 20 ºC. Measurements in short periods of time with low wind speed. 1 LID: first measurement with box, second measurement without the box, and third measurement the atmospheric contribution 2 LIDS: i) box with the “cold” lid, ii) box with the “hot” lid, and iii) T of the “hot” lid

1

1

2

1

t ss

t s

L L

L L

Lt1: radiance from the “hot” lid L1

s: radiance from the sample with the “cold” lid L2

s: radiance from the sample with the “hot” lid

Box with 2 lids

Angular Variations

Surface emissivity depends on different factors: -Composition of the body and spectral range -Temperature of the body (negligible for ambient temperatures) -Soil moisture (increases with SM) -Direction of emission (angular effects)

ANGULAR MEASUREMENTS

Expresión operativa para la emisividad direccionalabsoluta:

q =exp (- / T ) - 1,3 exp (- / T

exp (- / T ) - 1,3 exp (- / T )rad atm0

S atm0

)

Expresión operativa para la emisividad direccionalrelativa:

qr,

rad atm0

rad0 atm0

=exp (- / T ) - 1,3 exp (- / T

exp (- / T ) - 1,3 exp (- / T )

)

Absolute directional emissivity:

Relative directional emissivity:

(Factor 1.3: depends on the radiometer)

EXPERIMENTAL RESULTS

Semicircular goniometer with R=1.5 m Radiometer Omega OS86 (8-14 mm) with =0.1 K and IFOV=2º Thermopar (water measurements): TES 1310 Type K (=0.1 K) Thermistor calibrated in the laboratory with a Hg thermometer (Siebert&Kuhn, =0.05K) Samples: sand, clay, lime, gravel, water, grass Measurement steps: 5º (t< 2 min, thermal stability)

Samples

HOMOGENEOUS SAMPLES (8-14 mm)

sample

Decrease in

relative

emissivity

(%)

Decrease in

absolute

emissivity(%)

water 3,3 3,3

sand 2,0 1,9

clay 0,5 0,5

slime 0,9 0,9

gravel 1,2 1,2

grass 0 0

Difference at 0º and 55º

canal 1

0,940

0,960

0,980

1,000

0 20 40 60

ángulo (º)

r

ela

tiva

agua

arena

arcilla

limo

gravilla

canal 2

0,940

0,960

0,980

1,000

0 20 40 60

ángulo (º)

r

ela

tiva

agua

arena

arcilla

limo

gravilla

canal 3

0,940

0,960

0,980

1,000

0 20 40 60

ángulo (º)

r

ela

tiva

agua

arena

arcilla

limo

gravilla

canal 4

0,940

0,960

0,980

1,000

0 20 40 60

ángulo (º)

r

ela

tiva

agua

arena

arcilla

limo

gravilla

(Cuenca & Sobrino, 2004, Applied Optics)

HOMOGENEOUS SAMPLES (CIMEL BANDS)

(8-13 um)

(8-9 um) (10-11 um)

(11.5-12.5 um)

RESULTS FOR A WATER SAMPLE

agua: canal 1

0,950

0,960

0,970

0,980

0,990

1,000

1,010

0 20 40 60

ángulo (º)

re

lati

va

Masuda et al.

trabajo presente

agua: canal 2

0,950

0,960

0,970

0,980

0,990

1,000

1,010

0 20 40 60

ángulo (º)

r

ela

tiva

Masuda et al.

trabajo presente

agua: canal 3

0,950

0,960

0,970

0,980

0,990

1,000

1,010

0 20 40 60

ángulo (º)

r

ela

tiva

Masuda et al.

trabajo presente

agua: canal 4

0,950

0,960

0,970

0,980

0,990

1,000

1,010

0 20 40 60

ángulo (º)

r

ela

tiva

Masuda et al.

trabajo presente

Target

Automatic Goniometer

Green grass Wheat Bare soil

Angular measurements over different natural (agricultural) surfaces

Dn

iii LSBTn

LSBTLSBT1i

)( 1

- )( )( qqq

Angular variations on Brihtness Temperatures (LSBT: Land Surface Brightness Temperature)

Bare soil 0.00

2.00

4.00

6.00

8.00

10.00

-60 -40 -20 0 20 40 60

angle (º)

?T

(K

)

45.00

50.00

55.00

60.00

Tra

d (

ºC)

ΔT=T0-Tθ

T1 (ºC) Cim4

-3

-2

-1

0

1

2

3

-60 -40 -20 0 20 40 60

angle (º)

ΔLS

BT (K

)

C1 (8-13μm)

C2 (11,0-11,7μm)

C3 (10,3-11,0μm)

C4 (8,9-9,3μm)

C5 (8,5-8,9μm)

C6 (8,1-8,5μm)

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