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Optimal three dimensional launch vehicle trajectories with attitude and attitude rate constraintsMathematical models for optimal three dimensional launch vehicle trajectories with attitude and attitude rate constraints
Document ID
19690011448
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Spurlock, O. F. (NASA Lewis Research Center Cleveland, OH, United States)
Teren, F. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1969
Subject Category
Space Sciences
Report/Patent Number
NASA-TN-D-5117
Accession Number
69N20810
Funding Number(s)
CONTRACT_GRANT: 128-31-30-02-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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