s2e-core
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Add orbit interpolation method as an Orbit calculation feature
Details
We need a satellite orbit calculation method using interpolation with orbit time series input.
We already have a basic function as follows.
https://github.com/ut-issl/s2e-core/blob/develop/src/math_physics/orbit/interpolation_orbit.hpp
Closing conditions
The feature is implemented,
Supplementary information
NA
Note
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