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CR3BP, R2BP, and NBP orbits all have the same fields,r, v to represent some Cartesian position with respect to something. This should be standardized.
The motivation for this issue is some ideas I have for ephemeris wrappers. At first, I outputted TwoBodyState instances from the ephemeris files. But this isn't always valid! I'd like to use ephemeris for CR3BP, 2BP, and NBody analysis, as well as CR3BP and 2BP patched conics. So I should just output some Cartesian state that's valid across all modules.
Or maybe I should export Body instances?
Let's see what this turns into!
The text was updated successfully, but these errors were encountered:
CR3BP, R2BP, and NBP orbits all have the same fields,
r, v
to represent some Cartesian position with respect to something. This should be standardized.The motivation for this issue is some ideas I have for ephemeris wrappers. At first, I outputted
TwoBodyState
instances from the ephemeris files. But this isn't always valid! I'd like to use ephemeris for CR3BP, 2BP, and NBody analysis, as well as CR3BP and 2BP patched conics. So I should just output some Cartesian state that's valid across all modules.Or maybe I should export
Body
instances?Let's see what this turns into!
The text was updated successfully, but these errors were encountered: