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Optimal control applications for electrothermal multijet systems on synchronous earth spacecraftOptimal control applications for electrothermal multijet systems for attitude control and station keeping of 24-hour synchronous satellite
Document ID
19670024092
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Isley, W. C. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1967
Subject Category
Auxiliary Systems
Report/Patent Number
X-734-67-368
NASA-TM-X-55869
Report Number: X-734-67-368
Report Number: NASA-TM-X-55869
Accession Number
67N33421
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ATTITUDE CONTROL
THRUSTOR
SYNCHRONOUS SATELLITE
OPTIMAL CONTROL

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