Interface AttitudeProvider

    • Method Detail

      • getAttitude

        Attitude getAttitude​(PVCoordinatesProvider pvProv,
                             AbsoluteDate date,
                             Frame frame)
        Compute the attitude corresponding to an orbital state.
        Parameters:
        pvProv - local position-velocity provider around current date
        date - current date
        frame - reference frame from which attitude is computed
        Returns:
        attitude on the specified date and position-velocity state
      • getAttitude

        <T extends CalculusFieldElement<T>> FieldAttitude<T> getAttitude​(FieldPVCoordinatesProvider<T> pvProv,
                                                                         FieldAbsoluteDate<T> date,
                                                                         Frame frame)
        Compute the attitude corresponding to an orbital state.
        Type Parameters:
        T - type of the field elements
        Parameters:
        pvProv - local position-velocity provider around current date
        date - current date
        frame - reference frame from which attitude is computed
        Returns:
        attitude on the specified date and position-velocity state
        Since:
        9.0
      • getAttitudeRotation

        default Rotation getAttitudeRotation​(PVCoordinatesProvider pvProv,
                                             AbsoluteDate date,
                                             Frame frame)
        Compute the attitude-related rotation corresponding to an orbital state.
        Parameters:
        pvProv - local position-velocity provider around current date
        date - current date
        frame - reference frame from which attitude is computed
        Returns:
        attitude-related rotation on the specified date and position-velocity state
        Since:
        12.0
      • getAttitudeRotation

        default <T extends CalculusFieldElement<T>> FieldRotation<T> getAttitudeRotation​(FieldPVCoordinatesProvider<T> pvProv,
                                                                                         FieldAbsoluteDate<T> date,
                                                                                         Frame frame)
        Compute the attitude-related rotation corresponding to an orbital state.
        Type Parameters:
        T - type of the field elements
        Parameters:
        pvProv - local position-velocity provider around current date
        date - current date
        frame - reference frame from which attitude is computed
        Returns:
        rotation on the specified date and position-velocity state
        Since:
        12.0