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Classical eight- and lower-order Runge-Kutta-Nystroem formulas with stepsize control for special second-order differential equationsThe formulas include a stepsize control procedure, based on a complete coverage of the leading term of the truncation error in x. The formulas require fewer evaluations per stop than other Runge-Kutta-Nystrom formulas if the latter are operated by using the standard procedure for stepsize control. An example is presented. With results being of the same accuracy, Runge-Kutta-Nystrom formulas discussed save 50 percent or more computer time compared with other Runge-Kutta-Nystrom formulas.
Document ID
19720012011
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
March 1, 1972
Subject Category
Mathematics
Report/Patent Number
NASA-TR-R-381
M-533
Accession Number
72N19661
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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