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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
19670057281
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Scofield, H. N.
Date Acquired
August 3, 2013
Publication Date
August 1, 1967
Subject Category
Navigation
Report/Patent Number
AIAA PAPER 67-621
Report Number: AIAA PAPER 67-621
Accession Number
67A36010
Distribution Limits
Public
Copyright
Other
Keywords
COMPUTER METHOD
GUIDANCE AND CONTROL
ROCKET VEHICLE
AIRBORNE EQUIPMENT
ELLIPTICAL ORBIT

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