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Stabilization by modification of the LagrangianIn order to reduce the error growth during a numerical integration, a method of stabilization of the differential equations of the Keplerian motion is offered. It is characterized by the use of the eccentric anomaly as an independent variable in such a way that the time transformation is given by a generalized Lagrange formalism. The control terms in the equations of motion obtained by this modified Lagrangian give immediately a completely Liapunov-stable set of differential equations. In contrast to other publications, here the equation of time integration is modified by a control term which leads to an integral which defined the time element for the perturbed Keplerian motion.
Document ID
19760003089
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Baumgarte, J. W.
(Technische Univ. Brunswick, Germany)
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
Numerical Analysis
Accession Number
76N10177
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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