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Attitude Determination Error Analysis System (ADEAS) mathematical specifications documentThe mathematical specifications of Release 4.0 of the Attitude Determination Error Analysis System (ADEAS), which provides a general-purpose linear error analysis capability for various spacecraft attitude geometries and determination processes, are presented. The analytical basis of the system is presented. The analytical basis of the system is presented, and detailed equations are provided for both three-axis-stabilized and spin-stabilized attitude sensor models.
Document ID
19920018967
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Nicholson, Mark (Computer Sciences Corp. Lanham, MD, United States)
Markley, F. (Computer Sciences Corp. Lanham, MD, United States)
Seidewitz, E. (Computer Sciences Corp. Lanham, MD, United States)
Date Acquired
September 6, 2013
Publication Date
October 24, 1988
Subject Category
Numerical Analysis
Report/Patent Number
NASA-CR-189281
CSC/TM-88/6001
NAS 1.26:189281
Report Number: NASA-CR-189281
Report Number: CSC/TM-88/6001
Report Number: NAS 1.26:189281
Accession Number
92N28210
Funding Number(s)
CONTRACT_GRANT: NAS5-31500
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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