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

Function Documentation

State lupnt::CartToClassical(Real dt, const State &r1, const State &r2, Real GM)

Estimate classical orbital elements from two Cartesian position states.

Parameters:

  • dt – Time elapsed between r1 and r2.

  • r1 – First position state.

  • r2 – Second position state.

  • GM – Gravitational parameter consistent with the state units.

Returns:

Classical orbital element state.