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Propagator
In the Propagator::Propagate(const AbsoluteDate &toDate) function the orbit-rates needs to be updated.
Propagator::Propagate(const AbsoluteDate &toDate)
Currently using the propagator without drag effect consideration is acceptable, and results match well with the STK J2 Analytical Propagator.
The text was updated successfully, but these errors were encountered:
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In the
Propagator::Propagate(const AbsoluteDate &toDate)
function the orbit-rates needs to be updated.Currently using the propagator without drag effect consideration is acceptable, and results match well with the STK J2 Analytical Propagator.
The text was updated successfully, but these errors were encountered: