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lighting, aircraft, night vision imaging system - General Dynamics ...

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MIL-STD-3009<br />

x = 1931 C.I.E. relative spectral response of the eye<br />

(color matching function)<br />

y = 1931 C.I.E. relative spectral response of the eye<br />

(color matching function)<br />

z = 1931 C.I.E. relative spectral response of the eye<br />

(color matching function)<br />

X = C.I.E. tristimulus value<br />

Y = C.I.E. tristimulus value<br />

Z = C.I.E. tristimulus value<br />

u’ = 1976 UCS chromaticity coordinate transformation of CIE x<br />

v’ = 1976 UCS chromaticity coordinate transformation of CIE y<br />

x = 1931 C.I.E. chromaticity coordinate<br />

y = 1931 C.I.E. chromaticity coordinate<br />

5.7.11.2 Secondary <strong>lighting</strong> chromaticity measurements.<br />

For chromaticity measurements, the appropriate drive condition shall be applied to the<br />

light being tested (test light) to illuminate a reflectance standard meeting the<br />

requirements of APPENDIX A, to a luminance level of 0.343 cd/m 2 (0.1 fL) at a distance<br />

of 12 inches. The test light shall be oriented perpendicular to the reflectance standard.<br />

The spectroradiometer shall be set up such that the reflectance standard is at a 45°<br />

angle with the line of sight of the spectroradiometer. The spectral radiance of the<br />

reflectance standard shall be measured using an aperture that is as large as possible<br />

within the projected area of the reflectance standard. The corrected spectral radiance<br />

shall then be calculated using the following formula:<br />

N (λ) =<br />

Where:<br />

M( λ)<br />

r( λ)<br />

N(λ) = corrected spectral radiance (W/cm 2 sr nm)<br />

26<br />

(Formula 12)<br />

M(λ) = measured spectral radiance of the reflectance standard (W/cm 2 sr nm)

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