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When using the Encke propagator for an orbit of high eccentricity, for example e = 0.8, the root finder used by the Encke propagator does not converge in some cases. The attached file is a slightly changed version of singleSatellitePropagator.cpp that replicates the issue.
When using the Encke propagator for an orbit of high eccentricity, for example e = 0.8, the root finder used by the Encke propagator does not converge in some cases. The attached file is a slightly changed version of singleSatellitePropagator.cpp that replicates the issue.
singleSatellitePropagator.zip
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