Computer Science – Numerical Analysis
Scientific paper
Jun 1987
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1987cemec..40...95m&link_type=abstract
Celestial Mechanics (ISSN 0008-8714), vol. 40, no. 2, 1987, p. 95-110.
Computer Science
Numerical Analysis
Celestial Mechanics, Hypergeometric Functions, Numerical Analysis, Orbit Calculation, Two Body Problem, Computerized Simulation, Equations Of Motion, Libration, Many Body Problem, Numerical Integration, Orbital Mechanics
Scientific paper
A modification to the conventional polynomial extrapolation applied to the Gragg method (Gragg, 1965; Bulirsch and Stoer, 1966) is proposed which yields an arbitrary order solution and conserves the Jacobi motion constant. The modification yields a better approximation of the exact solution than convential polynomial extrapolation. The present method can be used to numerically determine the orbits near the colinear and triangular equilibrium points of any two-body system.
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