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A simplified explicit guidance scheme for orbital injection.Onboard computer equations for rocket vehicle guidance to elliptical orbit, discussing iteration absence from computations and digital simulation results
Document ID
19680064754
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Scofield, H. N.
Date Acquired
August 4, 2013
Publication Date
November 1, 1968
Subject Category
Navigation
Report/Patent Number
AIAA PAPER 67-621
Report Number: AIAA PAPER 67-621
Meeting Information
Meeting: GUIDANCE, CONTROL AND FLIGHT DYNAMICS CONFERENCE
Location: HUNTSVILLE, AL
Start Date: August 14, 1967
End Date: August 16, 1967
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
68A45726
Distribution Limits
Public
Copyright
Other

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