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An optimal discrete control strategy for interplanetary guidance.Guiding one state of linear dynamical system to prescribed rms terminal accuracy in presence of injection, measurement and engine-mechanization error
Document ID
19650051397
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Tung, F.
Date Acquired
August 2, 2013
Publication Date
July 1, 1965
Subject Category
Navigation
Accession Number
65A34101
Funding Number(s)
CONTRACT_GRANT: NAS1-3777
Distribution Limits
Public
Copyright
Other
Keywords
ROOT-MEAN-SQUARE ERROR
OPTIMAL CONTROL
INTERPLANETARY NAVIGATION
LINEAR SYSTEM

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