Orbits of the Kepler problem via polar reciprocals

Details Orbits of the Kepler problem via polar reciprocals Orbits of the Kepler problem via polar reciprocals

2011-07-05

arxiv.org/abs/1107.0852v1

American Journal of Physics, Volume 79, Issue 12, pp. 1246-1249 (2011)

Physics

Classical Physics

11 pages, 5 figures, accepted for publication by American Journal of Physics

Scientific paper

10.1119/1.3639130

It is argued that, for motion in a central force field, polar reciprocals of trajectories are an elegant alternative to hodographs. The principal advantage of polar reciprocals is that the transformation from a trajectory to its polar reciprocal is its own inverse. The form of polar reciprocals $k_*$ of Kepler problem orbits is established, and then the orbits $k$ themselves are shown to be conic sections using the fact that $k$ is the polar reciprocal of $k_*$. A geometrical construction is presented for the orbits of the Kepler problem starting from their polar reciprocals. No obscure knowledge of conics is required to demonstrate the validity of the method. Unlike a graphical procedure suggested by Feynman (and amended by Derbes), the algorithm based on polar reciprocals works without alteration for all three kinds of trajectories in the Kepler problem (elliptical, parabolic, and hyperbolic).

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