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

.. |SPACE_MOVER_MODEL| replace:: :model:`WSF_NORAD_SPACE_MOVER`

.. |SPACE_MOVER_SCRIPT_CLASS| replace:: :class:`WsfSpaceMover`

.. |SPACE_MOVER_MISSION_REF| replace:: :ref:`mission_sequence<WSF_NORAD_SPACE_MOVER.orbital_mission_sequence>`

.. |SPACE_MOVER_MANEUVERING_REF| replace:: :ref:`maneuvering models<WSF_NORAD_SPACE_MOVER.Maneuvering_Models>`

.. |SPACE_MOVER_ATTITUDE_REF| replace:: :ref:`attitude controller model<WSF_NORAD_SPACE_MOVER.Attitude_controller_Models>`

WSF_NORAD_SPACE_MOVER
---------------------

.. contents::
   :local:

**Script Type:** :class:`WsfSpaceMover`

.. model:: mover WSF_NORAD_SPACE_MOVER

.. parsed-literal::

   mover <name> :model:`WSF_NORAD_SPACE_MOVER`
      ... :command:`base mover commands <mover>`...
      ... `Orbital Element Commands`_...
      ... `Orbital Propagator Commands`_...

      orbit_color_ ...
      conjunction_setup_
         ...
      end_conjunction_setup
      :command:`attitude_controller` :ref:`<type-name><WSF_NORAD_SPACE_MOVER.Attitude_Controller_Models>` ...
         ...
      end_attitude_controller
      :command:`maneuvering`         :ref:`<type-name><WSF_NORAD_SPACE_MOVER.Maneuvering_Models>` ...
         ...
      end_maneuvering
      :ref:`mission_sequence<orbital_mission_sequence>`
         ...
      end_mission_sequence
	  
      orbital_state_ ... end_orbital_state
   end_mover

Overview
========

|SPACE_MOVER_MODEL| implements a mover for a platform in orbit about the Earth.  It is useful for modeling
satellites for which :command:`two-line element (TLE)<WSF_NORAD_SPACE_MOVER.orbit>` sets are available, including most operational Earth-orbiting satellites, non-operational satellites, and actively-tracked orbiting debris.

The mover implements propagation algorithms as defined in the document *SpaceTrack Report No. 3* (https://www.celestrak.com/NORAD/documentation/spacetrk.pdf) .  This report provides algorithms that define several models; the mover selects the appropriate model (NORAD SGP, SGP4, SGP8, SDP4, or SDP8) for propagation depending on the data provided in the two-line element.  Oblate earth, drag, and third-body Sun and Moon perturbation effects are taken into account by these models.

.. include:: space_mover_overview_common.txt

.. include:: space_mover_raan_inclination_note.txt

.. block:: WSF_NORAD_SPACE_MOVER

Commands
========

.. include:: orbital_state.txt

.. include:: orbit_color_commands.txt

.. _WSF_NORAD_SPACE_MOVER.Orbital_Element_Commands:

.. include:: two_line_element_commands.txt

.. _WSF_NORAD_SPACE_MOVER.Orbital_Propagator_Commands:

.. include:: orbital_propagator_commands.txt

.. _WSF_NORAD_SPACE_MOVER.Conjuntion_Input_Commands:

.. include:: conjunction_input.txt

.. _WSF_NORAD_SPACE_MOVER.Attitude_controller_Models:

.. include:: attitude_controller_models.txt

.. _WSF_NORAD_SPACE_MOVER.Maneuvering_Models:

.. include:: orbital_maneuvering_models.txt

.. _WSF_NORAD_SPACE_MOVER.orbital_mission_sequence:

.. include:: orbital_mission_sequence.txt

.. _WSF_NORAD_SPACE_MOVER.script_interface:

.. include:: space_mover_script_interface.txt