Length of arc as independent argument for highly eccentric orbits
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For analytic step regulation in numerical integration of highly eccentric orbits it is proposed to use the orbital arc length of a moving particle as independent argument.
[1] J. E. Glynn,et al. Numerical Recipes: The Art of Scientific Computing , 1989 .
[2] P. Nacozy. Time elements in Keplerian orbital elements , 1981 .
[3] Guy Janin. Accurate computation of highly eccentric satellite orbits , 1974 .
[4] José M. Ferrándiz. Linearization in special cases of perturbed Keplerian motions , 1986 .
[5] William H. Press,et al. Numerical recipes : the art of scientific computing : FORTRAN version , 1989 .