Efficient Orbit Integration by the Orbital Longitude Method Using Antifocal Anomaly

Details Efficient Orbit Integration by the Orbital Longitude Method Using Antifocal Anomaly Efficient Orbit Integration by the Orbital Longitude Method Using Antifocal Anomaly

Sep 2004

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2004aj....128.1455f&link_type=abstract

The Astronomical Journal, Volume 128, Issue 3, pp. 1455-1464.

Astronomy and Astrophysics

Astronomy

4

Celestial Mechanics, Methods: N-Body Simulations

Scientific paper

Adopting the antifocal anomaly as the basis of a new orbital longitude, we obtain a variation on the true-longitude method to numerically integrate perturbed Keplerian orbits. Although the new method is applicable to elliptical orbits only, it achieves a larger stability region and gives significantly smaller integration errors than the original method when the perturbations are small and the eccentricity is not too large.

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