poliastro.twobody.propagation.recseries¶
Module Contents¶
Classes¶
Kepler solver for elliptical orbits with recursive series approximation method. |
Attributes¶
- poliastro.twobody.propagation.recseries.__class__¶
- class poliastro.twobody.propagation.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¶
- propagate(self, state, tof)¶