American Journal of Environmental Engineering
p-ISSN: 2166-4633 e-ISSN: 2166-465X
2016; 6(4A): 119-128
doi:10.5923/s.ajee.201601.18

Silvia Beatriz Alves Rolim1, 2, Atilio Grondona3, Cristiano Lima Hackmann2, 4, Cristiano Rocha2
1Geosciences Institute, Federal University of Rio Grande do Sul, Porto Alegre-RS, Brazil
2Graduate Program in Remote Sensing, Federal University of Rio Grande do Sul, Porto Alegre-RS, Brazil
3Department of Engineering, College of Technology TecBrasil - Porto Alegre Unity, Porto Alegre-RS, Brazil
4Interdisciplinary Department in Science and Technology, Federal University of Rio Grande do Sul, Porto Alegre-RS, Brazil
Correspondence to: Silvia Beatriz Alves Rolim, Geosciences Institute, Federal University of Rio Grande do Sul, Porto Alegre-RS, Brazil.
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Copyright © 2016 Scientific & Academic Publishing. All Rights Reserved.
This work is licensed under the Creative Commons Attribution International License (CC BY).
http://creativecommons.org/licenses/by/4.0/

Remote data coming from the Thermal InfraRed (TIR) region of electromagnetic spectrum has several applications in geology, climatology, energy balance, biological and geophysical process analysis, disaster assessment and change detection analysis. In the TIR region, the emission of the targets is dominant when compared with reflection. This radiation is a function of two unknowns – the emissivity and the temperature of the target. To study TIR, a precise retrieval of the temperature and/or emissivity from the measured radiation is necessary. This process is usually difficult due to a non-linear relationship between these two unknowns and the measured radiation. In the last 40 years, several researchers have developed approaches to generate reliable results. However, all these methods have constraints in their applications. This paper reviews the advantages and disadvantages of the main methods of temperature and emissivity separation in order to create a summary that allows the researchers to choose the most suitable method in their own application.
Keywords: Thermal Infrared, Temperature Emissivity Separation, Temperature Retrieval, Emissivity Retrieval, TIR, TES
Cite this paper: Silvia Beatriz Alves Rolim, Atilio Grondona, Cristiano Lima Hackmann, Cristiano Rocha, A Review of Temperature and Emissivity Retrieval Methods: Applications and Restrictions, American Journal of Environmental Engineering, Vol. 6 No. 4A, 2016, pp. 119-128. doi: 10.5923/s.ajee.201601.18.
![]() | (1) |
is the radiation re-emitted by the blackbody,
is the wavelength (µm), T is the surface temperature (K),
is the first radiation constant and
is the second radiation constant .If the earth's surface were a perfect black body at a constant temperature and without the intervention of the atmosphere, the radiance measured at the sensor would be given by Equation (1). The targets do not emit radiance as a blackbody, and part of the absorbed energy is dissipated as thermal energy. The absorbed energy a body dissipates as thermal energy can be calculated as:![]() | (2) |
is the radiance measured at the sensor for wavelength and temperature disregarding the effects of the atmosphere. Equation (2) is a ratio of the radiance of a given material and the radiance of a blackbody under the same temperature and wavelength. Then, for any real material, and knowing the emissivity and the target's temperature, from the Equation 2 the radiance measured at the sensor can be written as:![]() | (3) |
![]() | (4) |
, and radiance measured by the sensor
. This non-linearity contributes to multiply the effects of atmospheric scattering, emission effects in scenes with more complex geometries, scenes with heterogeneity of the atmosphere, and scenes with different adjacent surfaces (Collins et al., 1999 and 2001).Due to the presence of the atmosphere, the radiance reaching the sensor should, most of the time, be corrected for the emission effects, atmospheric scattering and attenuation, before the application of some of the methods discussed in this paper. In the literature, the radiation measured at the sensor including the atmosphere contribution is,![]() | (5) |
![]() | (6) |
is the down-welling spectral radiance that strikes the Earth's surface from scattering and from the atmospheric emissions,
is the up-welling spectral radiance of the atmosphere that reaches the sensor,
is the spectral transmissivity of the atmosphere and
is the radiance measured in soil.In this work the main methods used by the scientific/academic community will be addressed, many of which served as the basis for newer and more complex methods. These methods are most applicable, because require less restrictions on the type of sensor, target, number of images and the number of spectral bands. There are other methods applied to more specific cases and will not be covered in this research. ![]() | (7) |
. Apparently, the problem of more variables than equations persists; however, the ratio
it is much less sensitive to small variations in the temperature that only the term
(For the range of land temperatures and wavelengths between 8-14μm). There are several ways to estimate the temperature from the thermal radiance, however, an independent method of the prior knowledge of the geology of the area is to reverse Equation (3) to calculate the brightness temperature
:![]() | (8) |
, as
. Thus
, where
represents the best estimate of the surface temperature.Considering the atmosphere's contribution, given by Equations (5) and (6), we have three possible cases:CASE 1 - Neglecting
the ratio in Equation (5) is: ![]() | (9) |
, which is valid for daily data, since the atmosphere is partially transparent in this spectral region, follows that the 2nd term of the sum
in Equation (9) can be neglected.CASE 2 – Including
, and if there is a large enough area for calibration as a body of water, for example, the upward radiance can be estimated, and the measured radiance, corrected. A residual error of upward spectral radiance introduces a secondary term in the last parenthesis of the Equation (9) with the form
. For data acquired in suborbital, this error level is less than or equal to
in Equation (9) and can be neglected.CASE 3 - With full atmospheric correction when the atmospheric parameters in Equation (6) can be estimated, the ratio of the corrected radiance, is given by:![]() | (10) |
![]() | (11) |
![]() | (12) |
, it was shown by Hardy et al. (1934) and Slater (1980) that the following approach for the Planck function is valid:![]() | (13) |
and
are constants related to band
and the temperature
. The band constants
and
are, respectively, given by:
Thus, from Equations (18), the band radiance
can be estimated to an approximate temperature
by:![]() | (14) |
. Now it is possible to rewrite Equation (12) as:![]() | (15) |
is the kinetic temperature.If, for each radiance, the term
can be neglected, Equation (15) becomes:![]() | (16.a) |
![]() | (16.b) |
![]() | (17.a) |
![]() | (17.b) |
and
the equation
. Using
and
the temperature on the left side of the Equations (17.a) and (17.b) can be eliminated. Using these equations, it is easy to define an independent index of temperature:![]() | (18.a) |
![]() | (18.b) |
![]() | (19) |
on Equation (19):
with:
where
and
where
being the highest surface temperature of brightness found between the bands for a given pixel. This temperature of choice is the best approach for the kinetic temperature, allowing calculating efficiently the term
.From this index
it is possible to calculate the spectral emissivity, only if we know the upward atmospheric radiance in all bands, and the emissivity of a reference band (Becker and Li, 1990).
of this band, it is possible to calculate an approximation of the surface temperature
for each pixel given from the measured radiance
using the inverse of Equations (5) and (6):![]() | (20) |
![]() | (21) |
where
is the referece emissivity,
is the radiance measured in band,
for pixel
, the terms
,
and
are, respectively, the upward radiance, the downward radiance and
is the atmospheric transmissivity for band
. Thus, the emissivity for pixel i is calculated by the equation,
with
being the highest temperature of the calculated temperatures for pixel i.![]() | (22) |
and wavelenghts close to
have maximum error of 1% (Siegel e Howell, 1982; Grondona et al., 2013). From the LR, arises the α-RM, which is an improved and simplified LR (Hook et al, 1992; Kealy and Hook, 1993; Gillespie et al, 1999), where the method's image-dependency is eliminated.Taking the average, over all bands of Equation (3) we have:![]() | (23) |
![]() | (24) |
![]() | (25) |
![]() | (26) |
is given by,![]() | (27) |
is the difference between the linearized equation of radiance and the radiance linearized average over all bands, for a particular pixel. Therefore, a set of temperature independent equations are obtained, and can be calculated using Equation (26) from the scene data. It should be noted that the alpha residues retain the shape of the emissivity spectrum but not its absolute value, and, for the purpose of laboratory data comparison (Equation (25)) with field data (Equation (26)), conversion of the former data should be performed. Using emissivity data obtained in laboratory, upon application in Equation (25) it is possible to calculate
, and then compare it with the scene data from Equation (26). However, to extract the emissivity of the scene directly from Equation (25), it is necessary to solve![]() | (28) |
However, the calculation of the emissivity in Equation (28) is not possible because
is not known. One way to calculate the variable
is considering the spectral behavior in the thermal infrared of common targets. Thus, from the variance of a set of various soil types, igneous rocks and sedimentary rocks, Equation (28) can be solved. To estimate the term
, a regression is used. Given by:![]() | (29) |
and the difference between maximum and minimum variation. Based on the average spectrum emissivity and using an iterative process, the mean emissivity is corrected by estimate according to the difference between the maximum value and minimum emissivity of the previous iteration. At the end of the process, the temperature is finally calculated. This process can be described in five steps (Matsunaga, 1994; Gillespie et al, 1999; Coll et al., 2007.):1. Initial estimate of emissivity spectra, usually with MNE.2. The MMD is calculated from the previous step for the first iteration, in the remaining, MMD is calculated from adjusted emissivity spectra as,![]() | (30) |
and
are, respectively, the maximum and minimum emissivities for the band
, at iteration
.3. The new average emissivity,
, is calculated using the expression![]() | (31) |
![]() | (32) |
and its respective radiance.The iterative process continues from step 2 to step 5 until the temperature difference between iterations is less than a predetermined number
, so that
.![]() | (33) |
![]() | (34) |
being the average emissivity for band
.The hypotheses of the Equations (33) and (34) are conceptually the same, but each one applies in a given situation. While the first serves for applications with a continuous spectrum, the second applies to spectrum intervals, in other words, the hypothesis of Equation (33) is wider than the case of Equation (34).Rewriting the radiance, as![]() | (35) |
it is an additive term with zero mean due to noise. Then the algorithm for estimates for the temperature
and emissivity
that minimizes the error
is given by, ![]() | (36) |
represents the real values of emissivity and temperature, while e and t are, respectively, the estimates of these variables. Expressing the terms e and t by:![]() | (37) |
![]() | (38) |
![]() | (39) |
, and, from this temperature, the first estimate for the emissivity
is calculated. Then, the new temperature to be used in the next iteration is calculated, and a revised estimate is made for the emissivity, and so on. The process iterates until the calculated temperature minimize the Equation (36), in other words:![]() | (40) |