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Trajectory computation by a hybrid computer for the Apollo midcourse abort simulation.Hybrid computer simulation for Apollo midcourse guidance from elliptical preabort orbit to another ellipse, using coplanar/noncoplanar orbit change guidance scheme
Document ID
19680034315
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Smith, C. L.
Date Acquired
August 4, 2013
Publication Date
August 1, 1967
Publication Information
Publisher: SIMULATION, VOL. 9, P. 81-87.
Subject Category
Computers
Accession Number
68A15287
Distribution Limits
Public
Copyright
Other

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