Specific detectivity

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^*=\frac{\sqrt{Af}}{NEP}, where A is the area of the photosensitive region of the detector and f is the frequency bandwidth. It is commonly expressed in Jones units (cm \cdot \sqrt{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 \mathfrak{R} (in units of A/W or V/W) and the noise spectral density S_n (in units of A/Hz^{1/2} or V/Hz^{1/2}) as NEP=\frac{S_n}{\mathfrak{R}}, it's common to see the specific detectivity expressed as D^*=\frac{\mathfrak{R}\cdot\sqrt{A}}{S_n}.

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^* = \frac{q\lambda \eta}{hc} \left[\frac{4kT}{R_0 A}+2q^2 \eta \Phi_b\right]^{-1/2}

With q as the electronic charge, \lambda is the wavelength of interest, h is Planck's constant, c is the speed of light, k is Boltzmann's constant, T is the temperature of the detector, R_0A is the zero-bias dynamic resistance area product (often measured experimentally, but also expressible in noise level assumptions), \eta is the quantum efficiency of the device, and \Phi_b is the total flux of the source (often a blackbody) in photons/sec/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 wavelet will be integrated over a given time constant over a given number of frames.

In detail, we compute the bandwidth \Delta fdirectly from the integration time constant t_c.

 \Delta f = \frac{1}{2 t_c}

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

 Signal_{rms} = \sqrt{\frac{1}{N}\big( \sum_i^{N} Signal_i^2 \big)}

 Noise_{rms} =\sigma^2= \sqrt{\frac{1}{N}\sum_i^N (Signal_i - Signal_{avg})^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 A_d 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 = \frac{Signal_{rms}}{H G} = \frac{Signal}{\int dH dA_d d\Omega_{BB}}

Where,

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

 NEP = \frac{Noise_{rms}}{R}  = \frac{Noise_{rms}}{Signal_{rms}}H G

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^* = \frac{\sqrt{\Delta f A_d}}{NEP} =  \frac{\sqrt{\Delta f A_d}}{H G} \frac{Signal_{rms}}{Noise_{rms}}

References

  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), doi:10.1364/JOSA.50.001058)

 This article incorporates public domain material from the General Services Administration document "Federal Standard 1037C".