.. _propagation_examples:

====================
Propagation
====================

Introductory examples
*********************

The following examples showcase the basic functionality of the Tudat numerical propagation framework, for both dynamics and the associated variational equations.

.. nbgallery::


  ./tudatpy-examples/propagation/keplerian_satellite_orbit.ipynb
  ./tudatpy-examples/propagation/perturbed_satellite_orbit.ipynb
  ./tudatpy-examples/propagation/linear_sensitivity_analysis.ipynb
  ./tudatpy-examples/propagation/solar_system_propagation.ipynb
  ./tudatpy-examples/propagation/thrust_between_Earth_Moon.ipynb
  ./tudatpy-examples/propagation/juice_flybys.ipynb
  ./tudatpy-examples/propagation/panelled_radiation_target.ipynb

Advanced examples
*********************

The following examples, some of the more advanced features of Tudat are showcased, using either custom functions for guidance, or a more complex definition of the equations of motion.
Note that an additional related example (in particular on the setup of a custom environment) can be found on the page for :ref:`asteroid_optimization_examples`.

.. nbgallery::

  ./tudatpy-examples/propagation/reentry_trajectory.ipynb
  ./tudatpy-examples/propagation/two_stage_rocket_ascent.ipynb
  ./tudatpy-examples/propagation/separation_satellites_diff_drag.ipynb
  ./tudatpy-examples/propagation/thrust_satellite_engine.ipynb
  ./tudatpy-examples/propagation/coupled_translational_rotational_dynamics.ipynb
  ./tudatpy-examples/propagation/impact_manifolds_lpo_cr3bp.ipynb