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A study of low-thrust guidance.Formulation of problem of guiding low thrust spacecraft back to nominal trajectory
Document ID
19670057278
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ash, G. R.
Dobrotin, B. M.
Date Acquired
August 3, 2013
Publication Date
August 1, 1967
Subject Category
Navigation
Report/Patent Number
AIAA PAPER 67-618
Report Number: AIAA PAPER 67-618
Accession Number
67A36007
Distribution Limits
Public
Copyright
Other
Keywords
TRAJECTORY CONTROL
TIME OPTIMAL CONTROL
CLOSED LOOP SYSTEM
SPACECRAFT GUIDANCE
ROCKET THRUST

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