An Orbital Element Formulation Without Solving Kepler's Equation

Details An Orbital Element Formulation Without Solving Kepler's Equation An Orbital Element Formulation Without Solving Kepler's Equation

Jan 2008

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2008aj....135...72f&link_type=abstract

The Astronomical Journal, Volume 135, Issue 1, pp. 72-82 (2008).

Astronomy and Astrophysics

Astronomy

2

Celestial Mechanics, Methods: Analytical, Methods: Numerical

Scientific paper

Starting from a standard orbital element formulation adopting the mean anomaly or longitude as the element related to time, changing its independent variable from the physical time to the corresponding eccentric angle, and replacing the mean angle with the time element of Stiefel & Scheifele, we present a new orbital element formulation of perturbed two-body problems which requires no solution of Kepler's equation.

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