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NONLINEAR GUIDANCE SYSTEM FOR DESCENT TRAJECTORIESOrbital mechanics applied to rocket engine vector and magnitude control in descent from orbit
Document ID
19630022683
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Shen, C. N.
Date Acquired
August 1, 2013
Publication Date
June 20, 1963
Subject Category
Space Radiation
Report/Patent Number
AIAA PAPER 63-151
Report Number: AIAA PAPER 63-151
Accession Number
63A18742
Funding Number(s)
CONTRACT_GRANT: NSG-14-59
Distribution Limits
Public
Copyright
Other
Keywords
GUIDANCE (MOTION)
MIDCOURSE GUIDANCE
ORBITAL MECHANICS
TERMINAL GUIDANCE

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