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The intermediate anomaly

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Abstract

A Sundman time transformation of the form

$$dt = cr^n ds$$

, wheren=3/2 andc is a constant, is integrated analytically for Keplerian motion. The integral involves an elliptic integral of the first kind. The variable s is called theintermediate anomaly.

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Authors and Affiliations

  1. University of Texas at Austin, 78712, Tex., USA

    Paul Nacozy

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  1. Paul Nacozy
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Nacozy, P. The intermediate anomaly. Celestial Mechanics 16, 309–313 (1977). https://doi.org/10.1007/BF01232657

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  • DOI: https://doi.org/10.1007/BF01232657

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