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Runge-Kutta Type Formulas of High-Order Accuracy and Their Application to the Numerical Integration of the Restricted Problem of Three BodiesRunge-Kutta type formulas applied to restricted three-body problem achieving high order accuracy by m-fold differentiation and simple transformation.
Document ID
19650036712
Acquisition Source
Marshall Space Flight Center
Document Type
Abstract
Authors
E Fehlberg (Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
August 2, 2013
Publication Date
January 1, 1964
Publication Information
Publication: Actes: Colloque International des Techniques de Calcul Analogique et Numerique en Aeronautique [Proceedings: International Symposium on Analogue and Digital Techniques Applied to Aeronautics]
Publisher: Presses Academiques Europeennes
Subject Category
Numerical Analysis
Meeting Information
Meeting: Colloque International Des Techniques de Calcul Analogique Et Numerique en Aeronautique
Location: Liège
Country: BE
Start Date: September 9, 1963
End Date: September 12, 1963
Sponsors: Association Internationale pour le Calcul Analogique
Accession Number
65A19416
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Runge-Kutta Integration
Differential Equation
Three-Body Problem

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IDRelationTitle19650036677Collected WorksActes: Colloque International des Techniques de Calcul Analogique et Numerique en Aeronautique [Proceedings: International Symposium on Analogue and Digital Techniques Applied to Aeronautics]
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