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The COMPACT Airborne Spectral Sensor (COMPASS) design is intended to demonstrate a new design concept for solar reflective hyper spectral systems for the Government. Capitalizing from recent focal plane developments, the COMPASS system utilizes a single FPA to cover the 0.4-2.35micrometers spectral region. This system also utilizes an Offner spectrometer design as well as an electron etched lithography curved grating technology pioneered by NASA/JPL. This paper also discusses the technical trades, which drove the design selection of COMPASS. When completed, the core COMPASS spectrometer design could be used in a large variety of configurations on a variety of aircraft.
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Christopher G. Simi
Edwin M. Winter
Mary M. Williams
Proceedings of SPIE, the International Society for Optical Engineering/Proceedings of SPIE
United States Army
Sensors (United States)
US Night Vision (United States)
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Simi et al. (Mon,) studied this question.
www.synapsesocial.com/papers/6a0fe15c9e54838161fd5449 — DOI: https://doi.org/10.1117/12.437000