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Numerical implications of stabilization by the use of integralsLiapunov or energy restraint methods for dynamic stabilization in two body motion perturbation problems are considered. Results of computerized orbital stabilization estimates show that the application of energy restraint prevents the occurrence of consistent timing errors in the stepwise integration of equations of motion for a nearly circular orbit.
Document ID
19760003095
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Beaudet, P. R.
(Computer Sciences Corp. Silver Spring, MD, United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1975
Publication Information
Publication: NASA. Goddard Space Flight Center Flight Mech.(Estimation Theory Symp.
Subject Category
Astrodynamics
Accession Number
76N10183
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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