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.
-
Updated
Apr 9, 2021 - Fortran
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.
This repository is for programs analyzing the habitability of the star system 30 Arietis.
Numerical integrator of orbits, including Yarkovsky effect, YORP, and collisions. Based on SWIFT (Levison & Duncan 1994).
Fortran library to compute positions of celestial bodies
N-body fortran integrator
Add a description, image, and links to the celestial-mechanics topic page so that developers can more easily learn about it.
To associate your repository with the celestial-mechanics topic, visit your repo's landing page and select "manage topics."