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A method of trajectory optimization by fast-time repetitive computationsPerturbation method of trajectory optimization by fast time repetitive computations of state equations
Document ID
19660012988
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Crane, D. F. (NASA Ames Research Center Moffett Field, CA, United States)
Raby, J. S. (NASA Ames Research Center Moffett Field, CA, United States)
Wingrove, R. C. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1966
Subject Category
Space Sciences
Report/Patent Number
NASA-TN-D-3404
Report Number: NASA-TN-D-3404
Accession Number
66N22277
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PERTURBATION THEORY
STATE EQUATION
COMPUTER PROGRAM
TRAJECTORY OPTIMIZATION
STEEPEST DESCENT METHOD

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