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Nonlinear feedback solution for minimum-time injection into circular orbit with constant thrust acceleration magnitudeNonlinear feedback solution for minimum-time injection into circular orbit with constant thrust acceleration magnitude
Document ID
19670007468
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bryson, A. E., Jr. (Harvard Univ. Cambridge, MA, United States)
Winfield, D. H. (Harvard Univ. Cambridge, MA, United States)
Date Acquired
August 3, 2013
Publication Date
July 1, 1966
Subject Category
Space Sciences
Report/Patent Number
NASA-CR-81474
TR-507
AD-641404
Report Number: NASA-CR-81474
Report Number: TR-507
Report Number: AD-641404
Accession Number
67N16797
Funding Number(s)
CONTRACT_GRANT: NONR-1866/16/
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DYNAMIC PROGRAMMING
SPACECRAFT TRAJECTORY
CIRCULAR ORBIT
NONLINEAR FEEDBACK

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