Analytic Central Orbits and their Transformation Group

Abstract

A useful crude approximation for Abelian functions is developed and applied to orbits. The bound orbits in the power-law potentials A*r-alpha take the simple form (l/r)k = 1 + e cos(m*phi), where k = 2 - alpha > 0 and 'l' and 'e' are generalisations of the semi-latus-rectum and the eccentricity. 'm' is given as a function of 'eccentricity'. For nearly circular orbits 'm' is sqrtk, while the above orbit becomes exact at the energy of escape where 'e' is one and 'm' is 'k'. Orbits in the logarithmic potential that gives rise to a constant circular velocity are derived via the limit of small alpha. For such orbits, r2 vibrates almost harmonically whatever the 'eccentricity'. Unbound orbits in power-law potentials are given in an appendix. The transformation of orbits in one potential to give orbits in a different potential is used to determine orbits in potentials that are positive powers of r. These transformations are extended to form a group which associates orbits in sets of six potentials, e.g. there are corresponding orbits in the potentials proportional to r, r-2/3, r-3, r-6, r4/3 and r-4. A degeneracy reduces this to three, which are r-1, r2 and r-4 for the Keplerian case. A generalisation of this group includes the isochrone with the Kepler set.

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