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Guidance analysis.Unmanned spacecraft guidance policy and orbit determination, using linear perturbation theory and minimum variance estimation
Document ID
19650030391
Acquisition Source
Legacy CDMS
Document Type
Book Chapter
Authors
Pfeiffer, C.
Date Acquired
August 2, 2013
Publication Date
January 1, 1964
Subject Category
Navigation
Accession Number
65A13095
Distribution Limits
Public
Copyright
Other
Keywords
SPACECRAFT GUIDANCE
TRAJECTORY CONTROL
UNMANNED SPACECRAFT
ORBIT CALCULATION

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