:orphan:

.. ****************************************************************************
.. CUI
..
.. The Advanced Framework for Simulation, Integration, and Modeling (AFSIM)
..
.. The use, dissemination or disclosure of data in this file is subject to
.. limitation or restriction. See accompanying README and LICENSE for details.
.. ****************************************************************************

Target
------

**Script Type:** :class:`WsfTargetManeuver`

.. parsed-literal::

   :ref:`maneuver<orbital_event.maneuver>` target
      :ref:`Common Maneuver Commands ...<orbital_event.common_commands>`
      delta_time_ ...
      maximum_delta_time_ ...
      maximum_delta_v_ ...
      optimize_time_ ...
      optimize_delta_v_ ...
      optimize_cost_ ...
      tolerance_ ...
      :doc:`target_specification` ...
   end_maneuver

.. block:: target_maneuver

Perform a maneuver to target (intercept with) the given platform.  Options are provided to optimize when the maneuver occurs, either at the earliest possible time, or with minimum delta-V expended during that time.

   .. note:: The script version of this maneuver, :class:`WsfTargetManeuver`, is used dynamically to target track locations.
   .. note:: Several conditions must be met before the maneuver can succeed.  These conditions include the following:

   * The platform must be valid at the start of the simulation.
   * The transfer orbit can only be hyperbolic if the mover executing the maneuver supports hyperbolic propagation.
   * The transfer orbit must not intersect earth.
   * When optimizing, a valid solution must exist for the provided optimization option (optimize_time_ or optimize_delta_v_).
   * The expended energy for the transfer must be less than the available delta-v.

.. include:: common_targeting_commands.txt