Special perturbation theory methods in celestial mechanics. II. Comparative analysis of numerical efficiency
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A comparative analysis of the efficiency of methods in special perturbation theory [1] is performed as applied to the numerical simulation of satellite, asteroid, and planetary orbits, and recommendations on their use are given.
[1] J. Butcher. Implicit Runge-Kutta processes , 1964 .
[2] E. Everhart. Implicit single-sequence methods for integrating orbits , 1974 .