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A TECHNIQUE FOR OPTIMUM FINAL VALUE CONTROL OF POWERED FLIGHT TRAJECTORIESTechnique for controlling the acceleration vector along a powered flight trajectory using a linear perturbation method
Document ID
19630022697
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Pfeiffer, C. G.
Date Acquired
August 1, 2013
Publication Date
June 20, 1963
Subject Category
Space Radiation
Report/Patent Number
AIAA PAPER 63-267
Report Number: AIAA PAPER 63-267
Accession Number
63A18756
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other
Keywords
TRAJECTORY CONTROL
FLIGHT PATH
CONTROL
OPTIMAL CONTROL

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