Function lupnt::CartToClassical(const State&, Real)

Function Documentation

State lupnt::CartToClassical(const State &rv, Real GM)

Convert a Cartesian position-velocity state to classical orbital elements.

Parameters:
  • rv – Cartesian state in the same distance/time units as GM.

  • GM – Gravitational parameter consistent with the state units.

Returns:

Classical orbital element state [a, e, i, RAAN, arg_periapsis, anomaly].