I am trying to build a tool that computes both the “time of closest approach” (TCA) and the “distance of closest approach” (DCA) of two spacecraft with respect to each other, using Orekit built-in functionality for Taylor Differential Algebra (to deal with uncertainty in initial conditions). The value of TCA, however, changes for every pair of new initial conditions around a nominal value. This is solved in bibliography by initializing the final time of integration as a DA (differential algebra) variable, and then evaluating the propagated polynomial for several values of the final integration time. Is there any way this can be done using orekit/hipparchus libraries with some modifications?
Thank you in advance. Regards,