boinor.twobody.propagation.recseries
====================================

.. py:module:: boinor.twobody.propagation.recseries

.. autoapi-nested-parse::

   module related to propagation of an orbit using the recursive series approximation method in the twobody sub-package



Classes
-------

.. autoapisummary::

   boinor.twobody.propagation.recseries.RecseriesPropagator


Module Contents
---------------

.. py:class:: RecseriesPropagator(method='rtol', order=8, numiter=100, rtol=1e-08)

   Kepler solver for elliptical orbits with recursive series approximation method.

   The order of the series is a user defined parameter.

   .. rubric:: Notes

   This algorithm uses series discussed in the paper *Recursive solution to
   Kepler's problem for elliptical orbits - application in robust
   Newton-Raphson and co-planar closest approach estimation*
   with DOI: http://dx.doi.org/10.13140/RG.2.2.18578.58563/1


   .. py:attribute:: kind


   .. py:method:: propagate(state, tof)

      actual propagation function for recseries propagator



   .. py:method:: propagate_many_sa(state, tofs)

      actual propagation function for recseries propagator with array of TOFs