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Nonlinear studies, optimal controlAttitude control for earth satellite in elliptic orbit, linearization in attitude control, and computation of optimal controls by method based on second variations
Document ID
19670006753
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Fluegge-Lotz, I. (Stanford Univ. CA, United States)
Date Acquired
August 3, 2013
Publication Date
December 1, 1966
Subject Category
Space Vehicles
Accession Number
67N16082
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LINEARIZATION
SATELLITE ATTITUDE CONTROL
ELLIPTICAL ORBIT
OPTIMAL CONTROL
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