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Earth orbit rendezvous evaluation programStudy program written in FORTRAN 4 developes an oribital rendezvous guidance scheme for large, constant thrust launch vehicles. It concentrates on /1/ an investigation of the direct extension of the present Saturn Iterative Guidance Mode /IGM/ scheme and /2/ a scheme formulated in a reference frame moving with the target satellite.
Document ID
19670000407
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Bennett, A. G.
Eskridge, C. D.
Hanafy, L. M.
Holm, G. L.
Omahony, M. L.
Quarles, J. D.
Date Acquired
August 3, 2013
Publication Date
November 1, 1967
Subject Category
Mathematics And Information Sciences
Report/Patent Number
MFS-13016
Report Number: MFS-13016
Accession Number
67B10407
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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