A C++ ROS package for real-time conversion of 3D motion controller events to ROS messages.

Versatile astrodynamics / space mission simulator. n-body orbital mechanics, maneuvers, perturbations and more.

Sample android Space Navigation View

The MATLAB model here presented performs trajectory propagations based on the Constant Density Polyhedron algorithm. With this model, it is possible to compute trajectories in the proximity of astronomical bodies such as asteroids or comets. The algorithm also allows to compute ballistic trajectories.