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Special Perturbations Using Back-Correction Methods of Numerical IntegrationA new class of linear multistep methods for numerical integration of differential equations is reported that permits satellite computation solutions to be corrected at certain points in the past as the integration advances in time. Algorithms have been developed for the solution of both first- and second-order differential equations. The back correction method appears to be more efficient than classical methods when dominant and perturbing forces can be separated.
Document ID
19760003096
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Feagin, T.
(Tennessee Univ. Space Inst. Tullahoma, TN, 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
76N10184
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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