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A technique for optimal final value control of powered flight trajectories.Technique for controlling acceleration vector along powered flight trajectory, using linear perturbation method
Document ID
19660042499
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Pfeiffer, C. G.
Date Acquired
August 3, 2013
Publication Date
February 1, 1966
Subject Category
Space Sciences
Report/Patent Number
AIAA PAPER 63-267
Report Number: AIAA PAPER 63-267
Accession Number
66A21789
Distribution Limits
Public
Copyright
Other
Keywords
TRAJECTORY CONTROL
OPTIMAL CONTROL

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