Function lupnt::InertialToSynodic

• Defined in File state_conversions.cc

Function Documentation

State lupnt::InertialToSynodic(const State &rv_c, const State &rv_d)

Convert two cartesian states to a relative RTN state.

Convert an inertial deputy state to a synodic state relative to a chief state.

Parameters:

• rv_c – Chief spacecraft state [km, km/s]

• rv_d – Deputy spacecraft state [km, km/s]

• rv_c – Chief inertial Cartesian state.

• rv_d – Deputy inertial Cartesian state.

Returns:

Relative RTN state [km, km/s]

Returns:

Deputy state in the chief-centered synodic frame.