.. default-domain:: java
.. highlight:: java
.. package:: krpc.client.services.SpaceCenter

Closest Approach
================


.. type:: public class ClosestApproach

   A close approach between an orbit and a target orbit. Obtained by calling
   :meth:`Orbit.nextClosestApproach(Orbit)` or :meth:`Orbit.closestApproaches(Orbit, int)`.

   .. note::

      A close approach is a snapshot: the time of closest approach is estimated once
      when the object is created, and every member describes the state at that time.
      Relative quantities are the target relative to the orbiting object (target minus
      self).

   .. method:: double getUT()


      The universal time of the closest approach, in seconds.

   

   .. method:: double getTimeTo()


      The time until the closest approach, in seconds.

   

   .. method:: double getDistance()


      The distance between the objects at the closest approach, in meters.

   

   .. method:: double getRelativeSpeed()


      The relative speed of the objects at the closest approach, in meters per
      second. This is the magnitude of :meth:`ClosestApproach.relativeVelocity(ReferenceFrame)`, and does
      not depend on the choice of reference frame.

   

   .. method:: Vessel getVessel()


      The vessel doing the approaching, or ``null`` if it is not a vessel.

   

   .. method:: CelestialBody getBody()


      The celestial body doing the approaching, or ``null`` if it is not a
      celestial body.

   

   .. method:: Vessel getTargetVessel()


      The vessel being approached, or ``null`` if the target is not a vessel.

   

   .. method:: CelestialBody getTargetBody()


      The celestial body being approached, or ``null`` if the target is not a
      celestial body.

   

   .. method:: org.javatuples.Triplet<Double,Double,Double> position(ReferenceFrame referenceFrame)

      The position of the orbiting object at the closest approach.

      :param ReferenceFrame referenceFrame: The reference frame that the returned position vector is in. Defaults to the orbital reference frame of the object the orbit belongs to.
      :returns: The position as a vector.
   

   .. method:: org.javatuples.Triplet<Double,Double,Double> targetPosition(ReferenceFrame referenceFrame)

      The position of the target object at the closest approach.

      :param ReferenceFrame referenceFrame: The reference frame that the returned position vector is in. Defaults to the orbital reference frame of the object the orbit belongs to.
      :returns: The position as a vector.
   

   .. method:: org.javatuples.Triplet<Double,Double,Double> velocity(ReferenceFrame referenceFrame)

      The velocity of the orbiting object at the closest approach.

      :param ReferenceFrame referenceFrame: The reference frame that the returned velocity vector is in. Defaults to the orbital reference frame of the object the orbit belongs to.
      :returns: The velocity as a vector.
   

   .. method:: org.javatuples.Triplet<Double,Double,Double> targetVelocity(ReferenceFrame referenceFrame)

      The velocity of the target object at the closest approach.

      :param ReferenceFrame referenceFrame: The reference frame that the returned velocity vector is in. Defaults to the orbital reference frame of the object the orbit belongs to.
      :returns: The velocity as a vector.
   

   .. method:: org.javatuples.Triplet<Double,Double,Double> relativePosition(ReferenceFrame referenceFrame)

      The position of the target relative to the orbiting object at the closest
      approach.

      :param ReferenceFrame referenceFrame: The reference frame whose axes the returned vector is expressed in. Defaults to the orbital reference frame of the object the orbit belongs to.
      :returns: The relative position as a vector.
   

   .. method:: org.javatuples.Triplet<Double,Double,Double> relativeVelocity(ReferenceFrame referenceFrame)

      The velocity of the target relative to the orbiting object at the closest
      approach.

      :param ReferenceFrame referenceFrame: The reference frame whose axes the returned vector is expressed in. Defaults to the orbital reference frame of the object the orbit belongs to.
      :returns: The relative velocity as a vector.