: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.
.. ****************************************************************************

Delta_V
-------

**Script Type:** :class:`WsfDeltaV_Maneuver`

.. parsed-literal::

   :ref:`maneuver<orbital_event.maneuver>` delta_v
      :ref:`Common Maneuver Commands ...<orbital_event.common_commands>`
      delta_v_ ...
   end_maneuver

A maneuver representing a change in the platform's ECI velocity.

.. command:: delta_v <frame> <speed-value> <speed-value> <speed-value>

   The desired change in the velocity of the platform, given in the specified orbital reference frame.

   The allowed value for the reference frame are:
    * **inertial** for a velocity change given in the inertial frame (typically the :ref:`ECI` frame, but this may represent equivalent frames for other central bodies if the platform is being evolved with a central body other than the Earth);
    * **ric** for a velocity change given in the executing platform's RIC frame.

.. command:: dv_x <speed-value>

   The desired change in the ECI x component of the velocity.

   .. note:: This command is deprecated. Please use delta_v_.

.. command:: dv_y <speed-value>

   The desired change in the ECI y component of the velocity.

   .. note:: This command is deprecated. Please use delta_v_.

.. command:: dv_z <speed-value>

   The desired change in the ECI z component of the velocity.

   .. note:: This command is deprecated. Please use delta_v_.