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Star tracker error analysis: Roll-to-pitch nonorthogonalityAn error analysis is described on an anomaly isolated in the star tracker software line of sight (LOS) rate test. The LOS rate cosine was found to be greater than one in certain cases which implied that either one or both of the star tracker measured end point unit vectors used to compute the LOS rate cosine had lengths greater than unity. The roll/pitch nonorthogonality matrix in the TNB CL module of the IMU software is examined as the source of error.
Document ID
19800004879
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Corson, R. W.
(McDonnell Douglas Technical Services Co., Inc.)
Date Acquired
September 4, 2013
Publication Date
October 1, 1979
Subject Category
Astrodynamics
Report/Patent Number
JSC-16238
REPT-79-FM-43
NASA-TM-80835
Report Number: JSC-16238
Report Number: REPT-79-FM-43
Report Number: NASA-TM-80835
Accession Number
80N13134
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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