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Direction-cosine attitude-control logic for spin-stabilized axisymmetric spacecraftDirection cosine attitude control logic for spin stabilized axisymmetric spacecraft, using control torques generated by reaction jet system
Document ID
19700063563
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Childs, D. W.
Date Acquired
August 5, 2013
Publication Date
August 1, 1970
Subject Category
Navigation
Accession Number
70A39679
Funding Number(s)
CONTRACT_GRANT: NGR-06-002-085
Distribution Limits
Public
Copyright
Other

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