poliastro.twobody.propagation.cowell
¶
Module Contents¶
Classes¶
Propagates orbit using Cowell's formulation. |
Attributes¶
- poliastro.twobody.propagation.cowell.__class__¶
- class poliastro.twobody.propagation.cowell.CowellPropagator(rtol=1e-11, events=None, f=func_twobody)¶
Propagates orbit using Cowell’s formulation.
Notes
This method uses the Dormand & Prince integration method of order 8(5,3) (DOP853). If multiple tofs are provided, the method propagates to the maximum value (unless a terminal event is defined) and calculates the other values via dense output.
- kind¶
- propagate(self, state, tof)¶
- propagate_many(self, state, tofs)¶