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Design and global analysis of spacecraft attitude control systemsMathematical model of global spacecraft attitude control system based on three dimensional motion
Document ID
19710009016
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Report (TR)
Authors
Meyer, G. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1971
Subject Category
Electronics
Report/Patent Number
A-3526
NASA-TR-R-361
Accession Number
71N18491
Funding Number(s)
CONTRACT_GRANT: 125-19-03-09-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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