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