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Determination of orbit of a spacecraft with respect to an object in a known circular orbitDifferential equations of motion of spacecraft in planetocentric orbit solved cylindrical shell coordinate system
Document ID
19660023726
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Dunning, R. S. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1966
Subject Category
Space Sciences
Report/Patent Number
NASA-TN-D-3518
Report Number: NASA-TN-D-3518
Accession Number
66N33016
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
COORDINATE SYSTEM
CYLINDRICAL SHELL
SPACECRAFT ORBIT
MOTION EQUATION
DIFFERENTIAL EQUATION

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