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Spacecraft attitude determination accuracy from mission experienceThis document presents a compilation of the attitude accuracy attained by a number of satellites that have been supported by the Flight Dynamics Facility (FDF) at Goddard Space Flight Center (GSFC). It starts with a general description of the factors that influence spacecraft attitude accuracy. After brief descriptions of the missions supported, it presents the attitude accuracy results for currently active and older missions, including both three-axis stabilized and spin-stabilized spacecraft. The attitude accuracy results are grouped by the sensor pair used to determine the attitudes. A supplementary section is also included, containing the results of theoretical computations of the effects of variation of sensor accuracy on overall attitude accuracy.
Document ID
19950006445
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Brasoveanu, D.
(Computer Sciences Corp. Lanham, MD., United States)
Hashmall, J.
(Computer Sciences Corp. Lanham, MD., United States)
Baker, D.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1994
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:104613
NASA-TM-104613
REPT-95B00001
Report Number: NAS 1.15:104613
Report Number: NASA-TM-104613
Report Number: REPT-95B00001
Accession Number
95N12858
Funding Number(s)
PROJECT: RTOP 550-00-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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