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'''Specific detectivity''', or '''''D*''''', for a [[photodetector]] is a [[figure of merit]] used to characterize performance, equal to the reciprocal of [[noise-equivalent power]] (NEP), normalized per square root of the sensor's area and frequency bandwidth (reciprocal of twice the integration time).
'''Specific detectivity''', or '''''D*''''', for a [[photodetector]] is a [[figure of merit]] used to characterize performance, equal to the reciprocal of [[noise-equivalent power]] (NEP), normalized per square root of the sensor's area and frequency bandwidth (reciprocal of twice the integration time).


Specific detectivity is given by <math>D^*=\frac{\sqrt{A \Delta f}}{NEP}</math>, where <math>A</math> is the area of the photosensitive region of the detector, <math>\Delta f</math> is the bandwidth, and NEP the noise equivalent power in units [W]. It is commonly expressed in ''Jones'' units (<math>cm \cdot \sqrt{Hz}/ W</math>) in honor of [[Robert Clark Jones]] who originally defined it.<ref>R. C. Jones, "Quantum efficiency of photoconductors," ''Proc. IRIS'' '''2''', 9 (1957)</ref><ref>R. C. Jones, "Proposal of the detectivity D** for detectors limited by radiation noise," ''J. Opt. Soc. Am.'' '''50''', 1058 (1960), {{doi|10.1364/JOSA.50.001058}})</ref>
Specific detectivity is given by <math>D^*=\frac{\sqrt{A \Delta f}}{NEP}</math>, where <math>A</math> is the area of the photosensitive region of the detector, <math>\Delta f</math> is the bandwidth, and NEP the noise equivalent power (in units of <math>W/\sqrt{Hz}</math>). It is commonly expressed in ''Jones'' units (<math>cm \cdot \sqrt{Hz}/ W</math>) in honor of [[Robert Clark Jones]] who originally defined it.<ref>R. C. Jones, "Quantum efficiency of photoconductors," ''Proc. IRIS'' '''2''', 9 (1957)</ref><ref>R. C. Jones, "Proposal of the detectivity D** for detectors limited by radiation noise," ''J. Opt. Soc. Am.'' '''50''', 1058 (1960), {{doi|10.1364/JOSA.50.001058}})</ref>


Given that noise-equivalent power can be expressed as a function of the [[responsivity]] <math>\mathfrak{R}</math> (in units of <math>A/W</math> or <math>V/W</math>) and the [[noise spectral density]] <math>S_n</math> (in units of <math>A/Hz^{1/2}</math> or <math>V/Hz^{1/2}</math>) as <math>NEP=\frac{S_n}{\mathfrak{R}}</math>, it is common to see the specific detectivity expressed as <math>D^*=\frac{\mathfrak{R}\cdot\sqrt{A}}{S_n}</math>.
Given that noise-equivalent power can be expressed as a function of the [[responsivity]] <math>\mathfrak{R}</math> (in units of <math>A/W</math> or <math>V/W</math>) and the [[noise spectral density]] <math>S_n</math> (in units of <math>A/Hz^{1/2}</math> or <math>V/Hz^{1/2}</math>) as <math>NEP=\frac{S_n \sqrt{\Delta f}}{\mathfrak{R}}</math>, it is common to see the specific detectivity expressed as <math>D^*=\frac{\mathfrak{R}\cdot\sqrt{A}}{S_n}</math>.


It is often useful to express the specific detectivity in terms of relative noise levels present in the device. A common expression is given below.
It is often useful to express the specific detectivity in terms of relative noise levels present in the device. A common expression is given below.
: <math>D^* = \frac{q\lambda \eta}{hc} \left[\frac{4kT}{R_0 A}+2q^2 \eta \Phi_b\right]^{-1/2}</math>
: <math>D^* = \frac{q\lambda \eta}{hc} \left[\frac{4kT}{R_0 A}+2q^2 \eta \Phi_b\right]^{-1/2}</math>


With ''q'' as the electronic charge, <math>\lambda</math> is the wavelength of interest, ''h'' is the Planck constant, ''c'' is the speed of light, ''k'' is the Boltzmann constant, ''T'' is the temperature of the detector, <math>R_0A</math> is the zero-bias dynamic resistance area product (often measured experimentally, but also expressible in noise level assumptions), <math>\eta</math> is the quantum efficiency of the device, and <math>\Phi_b</math> is the total flux of the source (often a blackbody) in photons/sec/cm<sup>2</sup>.
With <math>q</math> as the electronic charge, <math>\lambda</math> is the wavelength of interest, <math>h</math> is the [[Planck constant]], <math>c</math> is the [[speed of light]], <math>k</math> is the [[Boltzmann constant]], <math>T</math> is the temperature of the detector, <math>R_0A</math> is the zero-bias dynamic resistance area product (often measured experimentally, but also expressible in noise level assumptions), <math>\eta</math> is the [[quantum efficiency]] of the device, and <math>\Phi_b</math> is the total flux of the source (often a blackbody) in photons/s/cm<sup>2</sup>.


== Detectivity measurement ==
== Detectivity measurement ==
Detectivity can be measured from a suitable optical setup using known parameters.
Detectivity can be measured from a suitable optical setup using known parameters.
You will need a known light source with known irradiance at a given standoff distance. The incoming light source will be chopped at a certain frequency, and then each wavelength will be integrated over a given time constant over a given number of frames.
You will need a known light source with known irradiance at a given standoff distance. The incoming light source will be chopped at a certain frequency, and then each wavelength will be integrated over a given [[time constant]] over a given number of frames.


In detail, we compute the bandwidth <math>\Delta f</math> directly from the integration time constant <math>t_c</math>.
In detail, we compute the bandwidth <math>\Delta f</math> directly from the integration time constant <math>t_c</math>.
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: <math> \text{Noise}_{\text{rms}} = \sqrt{\frac{1}{N}\sum_i^N (\text{Signal}_i - \text{Signal}_{\text{avg}})^2} </math>
: <math> \text{Noise}_{\text{rms}} = \sqrt{\frac{1}{N}\sum_i^N (\text{Signal}_i - \text{Signal}_{\text{avg}})^2} </math>


Now, the computation of the radiance <math>H</math> in W/sr/cm<sup>2</sup> must be computed where cm<sup>2</sup> is the emitting area. Next, emitting area must be converted into a projected area and the [[solid angle]]; this product is often called the [[etendue]]. This step can be obviated by the use of a calibrated source, where the exact number of photons/s/cm<sup>2</sup> is known at the detector. If this is unknown, it can be estimated using the [[black-body radiation]] equation, detector active area <math>A_d</math> and the etendue. This ultimately converts the outgoing radiance of the black body in W/sr/cm<sup>2</sup> of emitting area into one of W observed on the detector.
Now, the computation of the radiance <math>H</math> in W/sr/cm<sup>2</sup> must be computed where cm<sup>2</sup> is the emitting area. Next, emitting area must be converted into a [[projected area]] and the [[solid angle]]; this product is often called the [[etendue]]. This step can be obviated by the use of a calibrated source, where the exact number of photons/s/cm<sup>2</sup> is known at the detector. If this is unknown, it can be estimated using the [[black-body radiation]] equation, detector active area <math>A_d</math> and the etendue. This ultimately converts the outgoing radiance of the black body in W/sr/cm<sup>2</sup> of emitting area into one of W observed on the detector.


The broad-band responsivity, is then just the signal weighted by this wattage.
The broad-band responsivity, is then just the signal weighted by this wattage.
: <math>R = \frac{\text{Signal}_{\text{avg}}}{H G} = \frac{\text{Signal}_{\text{avg}}}{\int dH dA_d d\Omega_{BB}},</math>
: <math>R = \frac{\text{Signal}_{\text{avg}}}{H G} = \frac{\text{Signal}_{\text{avg}}}{\int dH dA_d d\Omega_{BB}},</math>
where
where
* <math>R</math> is the responsivity in units of Signal / W, (or sometimes V/W or A/W)
* <math>R</math> is the responsivity in units of Signal / W, (or sometimes V/W or A/W),
* <math>H</math> is the outgoing radiance from the black body (or light source) in W/sr/cm<sup>2</sup> of emitting area
* <math>H</math> is the outgoing radiance from the black body (or light source) in W/sr/cm<sup>2</sup> of emitting area,
* <math>G</math> is the total integrated etendue between the emitting source and detector surface
* <math>G</math> is the total integrated etendue between the emitting source and detector surface,
* <math>A_d</math> is the detector area
* <math>A_d</math> is the detector area,
* <math>\Omega_{BB}</math> is the solid angle of the source projected along the line connecting it to the detector surface.
* <math>\Omega_{BB}</math> is the solid angle of the source projected along the line connecting it to the detector surface.



Latest revision as of 20:47, 19 May 2026

Template:Short description Template:Third-party Specific detectivity, or D*, for a photodetector is a figure of merit used to characterize performance, equal to the reciprocal of noise-equivalent power (NEP), normalized per square root of the sensor's area and frequency bandwidth (reciprocal of twice the integration time).

Specific detectivity is given by D*=AΔfNEP, where A is the area of the photosensitive region of the detector, Δf is the bandwidth, and NEP the noise equivalent power (in units of W/Hz). It is commonly expressed in Jones units (cm⋅Hz/W) in honor of Robert Clark Jones who originally defined it.[1][2]

Given that noise-equivalent power can be expressed as a function of the responsivity ℜ (in units of A/W or V/W) and the noise spectral density Sn (in units of A/Hz1/2 or V/Hz1/2) as NEP=SnΔfℜ, it is common to see the specific detectivity expressed as D*=ℜ⋅ASn.

It is often useful to express the specific detectivity in terms of relative noise levels present in the device. A common expression is given below.

D*=qληhc[4kTR0A+2q2ηΦb]−1/2

With q as the electronic charge, λ is the wavelength of interest, h is the Planck constant, c is the speed of light, k is the Boltzmann constant, T is the temperature of the detector, R0A is the zero-bias dynamic resistance area product (often measured experimentally, but also expressible in noise level assumptions), η is the quantum efficiency of the device, and Φb is the total flux of the source (often a blackbody) in photons/s/cm2.

Detectivity measurement

Detectivity can be measured from a suitable optical setup using known parameters. You will need a known light source with known irradiance at a given standoff distance. The incoming light source will be chopped at a certain frequency, and then each wavelength will be integrated over a given time constant over a given number of frames.

In detail, we compute the bandwidth Δf directly from the integration time constant tc.

Δf=12tc

Next, an average signal and rms noise needs to be measured from a set of N frames. This is done either directly by the instrument, or done as post-processing.

Signalavg=1N(∑iNSignali)
Noiserms=1N∑iN(Signali−Signalavg)2

Now, the computation of the radiance H in W/sr/cm2 must be computed where cm2 is the emitting area. Next, emitting area must be converted into a projected area and the solid angle; this product is often called the etendue. This step can be obviated by the use of a calibrated source, where the exact number of photons/s/cm2 is known at the detector. If this is unknown, it can be estimated using the black-body radiation equation, detector active area Ad and the etendue. This ultimately converts the outgoing radiance of the black body in W/sr/cm2 of emitting area into one of W observed on the detector.

The broad-band responsivity, is then just the signal weighted by this wattage.

R=SignalavgHG=Signalavg∫dHdAddΩBB,

where

  • R is the responsivity in units of Signal / W, (or sometimes V/W or A/W),
  • H is the outgoing radiance from the black body (or light source) in W/sr/cm2 of emitting area,
  • G is the total integrated etendue between the emitting source and detector surface,
  • Ad is the detector area,
  • ΩBB is the solid angle of the source projected along the line connecting it to the detector surface.

From this metric noise-equivalent power can be computed by taking the noise level over the responsivity.

NEP=NoisermsR=NoisermsSignalavgHG

Similarly, noise-equivalent irradiance can be computed using the responsivity in units of photons/s/W instead of in units of the signal. Now, the detectivity is simply the noise-equivalent power normalized to the bandwidth and detector area.

D*=ΔfAdNEP=ΔfAdHGSignalavgNoiserms

See also

References

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  1. ↑ R. C. Jones, "Quantum efficiency of photoconductors," Proc. IRIS 2, 9 (1957)
  2. ↑ R. C. Jones, "Proposal of the detectivity D** for detectors limited by radiation noise," J. Opt. Soc. Am. 50, 1058 (1960), Script error: No such module "CS1 identifiers".)

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