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It would be nice if a couple new factory functions were added for the creation of MGA transfers:
Directly define an initial/final state for the transfer: currently the initial/final state comes from the state of the departure/arrival body, it should also be possible to select initial/final states not associated with any body. Could be useful for validation purposes, e.g. to compare with the thrust arcs of some mission (@sbcowan 😁 ). Right now this can be circumvented by defining the departure/arrival bodies with user-specified constant ephemerides and a dummy gravitational parameter.
Allow the definition of departure/arrival orbits e.g. for Earth-centered transfers. Right now this can be circumvented by defining the departure/arrival bodies with the desired orbits and a dummy gravitational parameter.
The text was updated successfully, but these errors were encountered:
Hi all,
It would be nice if a couple new factory functions were added for the creation of MGA transfers:
The text was updated successfully, but these errors were encountered: