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Optical rate sensor algorithmsOptical sensors, in particular Charge Coupled Device (CCD) arrays, will be used on Space Station to track stars in order to provide inertial attitude reference. Algorithms are presented to derive attitude rate from the optical sensors. The first algorithm is a recursive differentiator. A variance reduction factor (VRF) of 0.0228 was achieved with a rise time of 10 samples. A VRF of 0.2522 gives a rise time of 4 samples. The second algorithm is based on the direct manipulation of the pixel intensity outputs of the sensor. In 1-dimensional simulations, the derived rate was with 0.07 percent of the actual rate in the presence of additive Gaussian noise with a signal to noise ratio of 60 dB.
Document ID
19900015681
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Uhde-Lacovara, Jo A.
(Stevens Inst. of Tech. Hoboken, NJ, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1989
Publication Information
Publication: Texas A&M Univ., NASA(ASEE Summer Faculty Fellowship Program, 1989, Volume 2
Subject Category
Optics
Accession Number
90N24997
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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