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Optimal guidance for ascent trajectories into circular orbits.Optimal guidance equations for ascent trajectories into circular orbits, developing feedback guidance loop for real onboard control system
Document ID
19670039766
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Pines, S.
Date Acquired
August 3, 2013
Publication Date
January 1, 1967
Subject Category
Navigation
Report/Patent Number
AIAA PAPER 67-56
Report Number: AIAA PAPER 67-56
Accession Number
67A18495
Funding Number(s)
CONTRACT_GRANT: NAS12-114
CONTRACT_GRANT: NAS9-4036
Distribution Limits
Public
Copyright
Other
Keywords
ASCENT TRAJECTORY
FEEDBACK CONTROL SYSTEM
CIRCULAR ORBIT
OPTIMIZATION
GUIDANCE AND CONTROL

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