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Classical eighth- and lower-order Runge-Kutta-Nystroem formulas with a new stepsize control procedure for special second-order differential equationsNew Runge-Kutta-Nystrom formulas of the eighth, seventh, sixth, and fifth order are derived for the special second-order (vector) differential equation x = f (t,x). In contrast to Runge-Kutta-Nystrom formulas of an earlier NASA report, these formulas provide a stepsize control procedure based on the leading term of the local truncation error in x. This new procedure is more accurate than the earlier Runge-Kutta-Nystrom procedure (with stepsize control based on the leading term of the local truncation error in x) when integrating close to singularities. Two central orbits are presented as examples. For these orbits, the accuracy and speed of the formulas of this report are compared with those of Runge-Kutta-Nystrom and Runge-Kutta formulas of earlier NASA reports.
Document ID
19730015887
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Report (TR)
Authors
Fehlberg, E.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1973
Subject Category
Mathematics
Report/Patent Number
M-544
NASA-TR-R-410
Accession Number
73N24614
Funding Number(s)
PROJECT: RTOP 014-00-00-00-62
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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