Function lupnt::ClassicalToCart

• Defined in File state_conversions.h

Function Documentation

State lupnt::ClassicalToCart(const State &coe, Real GM)

Convert classical orbital elements to Cartesian position and velocity.

Parameters:

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

• GM – Gravitational parameter consistent with the semi-major-axis units.

Returns:

Cartesian state in the same frame as coe.