A fifth alaebraic order trigonometrically-fitted modified Runge-Kutta Zonneveld method for the numerical solution of orbital problems
A trigonometrically-fitted Runge-Kutta method for the numerical integration of orbital problems is developed. Theoretical and numerical results obtained for some well-known orbital problems show the efficiency of the method. (c) 2005 Elsevier Ltd. All rights reserved.
trigonometrically-fitting orbital problems runge-kutta methods exponential-fitting