OrekitIllegalArgumentException using SRP, third body forces in DSST progator
Dear Orekit developers I have an issue while using different DSST force models for Solar Radiation Pressure, Third body perturbation of Sun and Moon. I get the following exception: org.orekit.errors.OrekitIllegalArgumentException: hyperbolic orbits cannot be handled as org.orekit.orbits.EquinoctialOrbit instances
Using DSSTTesseral and DSSTZonal I don't get any exception. I dug deeper and saw that a pseudo inertial frame was needed at a point in the routine StateMapper, so I changed from FramesFactory.getITRF to TIRF. But this change didn't help. I also read some of the old issues but couldn't solve my issue with this exception. I tried to see the difference using Numerical propagator instead and noticed there was no exception in case of Numerical propagator. Could you please tell me if I overlooked something or if something needs to be corrected. I also attached the file that I am talking about.
Thanks a lot!