Tudat/Astrodynamics/BasicAstrodynamics/missionGeometry.cpp
//! Compute whether an orbit is retrograde based on Keplerian state.
Compute whether an orbit is retrograde based on Keplerian state.
Compute whether an orbit is retrograde based on Keplerian state .
bool isOrbitRetrograde( const Eigen::Vector6d& keplerElements )
{
    return isOrbitRetrograde(
                keplerElements(
                    orbital_element_conversions::inclinationIndex ) );
}
bool isOrbitRetrograde ( const Eigen :: Vector6d & keplerElements ) { return isOrbitRetrograde ( keplerElements ( orbital_element_conversions :: inclinationIndex ) ) ; }
Compute whether an orbit is retrograde based on Keplerian state.
Compute whether an orbit is retrograde based on Keplerian state .
// Get inclination from vector and call overloaded function.