USA As Represented by Secretary of the Navy

Michael J Wilson

Thomas G Giallorenzi

Michael K Yetzbacher

A camera system includes a mosaic optical color filter array, which includes a plurality of repeating unit cells that enforce spectral consistency and spatial uniformity. Each repeating unit cell of the plurality of repeating unit cells satisfies a minimum focal-plane array perimeter criterion and a minimum perimeter to area ratio criterion. The spatial arrangement of bands within the repeating unit cell minimizes inter-band correlation between nearest neighbors. The camera system further includes as short-wave infrared detector optically coupled to the mosaic optical color filter array. Optionally, the mosaic optical color filter array includes at least five spectral bands. The plurality of repeating unit cells includes the at least five spectral bands.

Multiple band short wave infrared mosaic array filter

Micro-spectral sensors and methods are presented in which a Fizeau wedge interference filter is disposed between a focal plane array and a visible scene with an increasing wedge filter dimension varying along a scan direction, where the scene is scanned along the FPA to obtain light intensity measurements of a given scene location at different times using different FPA sensor elements through different wedge filter thicknesses, and the measurements correlated to the given scene location are Fourier transform to generate spectral data for the location.

Micro-spectral sensor

A system and method for performing attitude determination for projectiles comprises a projectile; a plurality of magnetometers arranged orthogonally to one another in the projectile, wherein the plurality of magnetometers are adapted to take first flight vector measurements of the projectile; a plurality of angular rate sensors in the projectile and proximate to the plurality of magnetometers, wherein the plurality of angular rate sensors are adapted to take second flight vector measurements of the projectile; a digital signal processor adapted to combine the first and second flight vector measurements to estimate Euler angles associated with a position of the projectile; and a calculator adapted to determine an attitude of the projectile based on the estimated Euler angles. Preferably, the plurality of magnetometers comprises three magnetometers aligned within the projectile, and wherein a first one of the magnetometers is aligned with a spin axis of the projectile.

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Middletown, DE, United States of America

Michael J Wilson