DSST Third Body Sun Perturbation leads to hyperbolic trajectory
I am using the DSST propagator on a Galileo-like orbit.
When I switch ON the third body perturbation for Sun, I've got a
propagation error (hyperbolic trajectory) even on a short propagation
duration (one day).
And no problem when the third body perturbation for the Sun is switched OFF.
I think there is a bug somewhere in DSSTThirdBody.
See the small test case here attached.
Could you please analyze this problem ?
(from redmine: issue id 478, created on 2018-06-18)