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NASA NTRS · 19830031710

Geometrically derived difference formulae for the numerical integration of trajectory problems

Abstract

An initial value problem for the autonomous system of ordinary differential equations dy/dt = f(y), where y is a vector, is considered. In a number of practical applications the interest lies in obtaining the curve traced by the solution y. These applications include the computation of trajectories in mechanical problems. The term 'trajectory problem' is employed to refer to these cases. Lambert and McLeod (1979) have introduced a method involving local rotation of the axes in the y-plane for the two-dimensional case. The present investigation continues the study of difference schemes specifically derived for trajectory problems. A simple geometrical way of constructing such methods is presented, and the local accuracy of the schemes is investigated. A circularly exact, fixed-step predictor-corrector algorithm is defined, and a variable-step version of a circularly exact algorithm is presented.

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BibTeXRIS

Mcleod, R. J. Y., Sanz-Serna, J. M.. 1982-07-01. Geometrically derived difference formulae for the numerical integration of trajectory problems. https://ntrs.nasa.gov/citations/19830031710

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