poliastro2.core.actions.propagate.recseries

Classes

RecseriesPropagator([method, order, ...])

Kepler solver for elliptical orbits with recursive series approximation method.

class poliastro2.core.actions.propagate.recseries.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.

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

kind = 1

propagate(state, tof)