Class GroundPointing

    • Constructor Detail

      • GroundPointing

        protected GroundPointing​(Frame inertialFrame,
                                 Frame bodyFrame)
        Default constructor. Build a new instance with arbitrary default elements.
        Parameters:
        inertialFrame - frame in which orbital velocities are computed
        bodyFrame - the frame that rotates with the body
        Since:
        7.1
    • Method Detail

      • getBodyFrame

        public Frame getBodyFrame()
        Get the body frame.
        Returns:
        body frame
      • getTargetPV

        protected abstract TimeStampedPVCoordinates getTargetPV​(PVCoordinatesProvider pvProv,
                                                                AbsoluteDate date,
                                                                Frame frame)
        Compute the target point position/velocity in specified frame.
        Parameters:
        pvProv - provider for PV coordinates
        date - date at which target point is requested
        frame - frame in which observed ground point should be provided
        Returns:
        observed ground point position (element 0) and velocity (at index 1) in specified frame
      • getTargetPV

        protected abstract <T extends CalculusFieldElement<T>> TimeStampedFieldPVCoordinates<T> getTargetPV​(FieldPVCoordinatesProvider<T> pvProv,
                                                                                                            FieldAbsoluteDate<T> date,
                                                                                                            Frame frame)
        Compute the target point position/velocity in specified frame.
        Type Parameters:
        T - type of the field elements
        Parameters:
        pvProv - provider for PV coordinates
        date - date at which target point is requested
        frame - frame in which observed ground point should be provided
        Returns:
        observed ground point position (element 0) and velocity (at index 1) in specified frame
        Since:
        9.0
      • getTargetPosition

        protected Vector3D getTargetPosition​(PVCoordinatesProvider pvProv,
                                             AbsoluteDate date,
                                             Frame frame)
        Compute the target point position in specified frame.
        Parameters:
        pvProv - provider for PV coordinates
        date - date at which target point is requested
        frame - frame in which observed ground point should be provided
        Returns:
        observed ground point position in specified frame
        Since:
        12.0
      • getTargetPosition

        protected <T extends CalculusFieldElement<T>> FieldVector3D<T> getTargetPosition​(FieldPVCoordinatesProvider<T> pvProv,
                                                                                         FieldAbsoluteDate<T> date,
                                                                                         Frame frame)
        Compute the target point position in specified frame.
        Type Parameters:
        T - type of the field elements
        Parameters:
        pvProv - provider for PV coordinates
        date - date at which target point is requested
        frame - frame in which observed ground point should be provided
        Returns:
        observed ground point position in specified frame
        Since:
        12.0
      • getAttitude

        public Attitude getAttitude​(PVCoordinatesProvider pvProv,
                                    AbsoluteDate date,
                                    Frame frame)
        Compute the attitude corresponding to an orbital state.
        Specified by:
        getAttitude in interface AttitudeProvider
        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

        public <T extends CalculusFieldElement<T>> FieldAttitude<T> getAttitude​(FieldPVCoordinatesProvider<T> pvProv,
                                                                                FieldAbsoluteDate<T> date,
                                                                                Frame frame)
        Compute the attitude corresponding to an orbital state.
        Specified by:
        getAttitude in interface AttitudeProvider
        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
      • getAttitudeRotation

        public Rotation getAttitudeRotation​(PVCoordinatesProvider pvProv,
                                            AbsoluteDate date,
                                            Frame frame)
        Compute the attitude-related rotation corresponding to an orbital state.
        Specified by:
        getAttitudeRotation in interface AttitudeProvider
        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
      • getAttitudeRotation

        public <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.
        Specified by:
        getAttitudeRotation in interface AttitudeProvider
        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