Propagation#
Introductory examples#
The following examples showcase the basic functionality of the Tudat numerical propagation framework, for both dynamics and the associated variational equations.
Keplerian satellite orbit
Perturbed satellite orbit
Linear sensitivity analysis using variational equations
Solar System Propagation using Multi-Body Dynamics
Thrust between the Earth and the Moon
JUICE Flybys of Jovian Moons
Setup a Panelled Radiation Pressure Model
Walker constellation propagation
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 Asteroid Orbit Optimization.
