This application allows you to generate lists of astronomical objects that can be seen from your location.

Physical systems with Newtonian gravity

The interface to the catalog of three-body and two-body mean-motion resonances

This repository contains the code for the blog post on Runge-Kutta methods for solving ODEs. For further details, please refer to this post.

Проект по ИД "Небесна Механика" към ФМИ, СУ

Easy-to-use minor planet orbit propagator with animated orbits

This repository is for programs analyzing the habitability of the star system 30 Arietis.

Presentations on some of the computer methods considered in the course

Finding the stable orbits of a small comet in a comet–earth–sun 3 body system using the classic Runge–Kutta method as well as the concept of Lagrange points.

Небесна механика / Nebesna mehanika

D translation of the libnova celestial mechanics engine.

A Python turtle simulation of planet movements to study Kepler's laws and how they emerge from Newton's law of gravity, for high school or lower level undergraduate students. Also, a slide show.

N-body model of Saturn and some of its moons with python.

FYS2085 project work: planetary motion

Finding a figure-8 solution to a three-body problem with arbitrary precision

Modelling dynamics of main-belt asteroids

Celestial Mechanics

ODE solvers for celestial mechanics

Calculates an ephemeris of a celestial object provided its orbital elements, observation date, and returns it as declination and right ascension

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.