A NEW EIGHT-STEP SYMMETRIC EMBEDDED PREDICTOR-CORRECTOR METHOD (EPCM) FOR ORBITAL PROBLEMS AND RELATED IVPs WITH OSCILLATORY SOLUTIONS
Author:
Publisher
American Astronomical Society
Subject
Space and Planetary Science,Astronomy and Astrophysics
Link
http://stacks.iop.org/1538-3881/145/i=3/a=75/pdf
Reference20 articles.
1. A one-step method for direct integration of structural dynamic equations
2. Symmetric linear multistep methods
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