Multi-rendezvous Spacecraft Trajectory Optimization with Beam P-ACO

A proof-of-concept for building Orbiter spaceflight simulator addons in Rust

Spacecraft atmospheric entry simulations using Python

ParaView template project for orbital data visualization (orbits, trajectory points, ground station field of view)

Capstone project for Spacecraft Dynamics and Control course

A quick-and-dirty SQL database for storing the historical orbital elements of satellites, including a script for trawling data from Celestrak and Space Track to populate the database.

Fast, accessible, accurate orbit propagator for spacecraft

A library to track spacecraft, written in C/C++

Software development and engineering project for solving the spacecraft-moon-Earth three-body problem.

Trajectory optimization tools for lunar missions

Designing an interplanetary trajectory to planet Mars 🌕

A tool for planning flights from one celestial body in KSP to another

space debris re-entty calc

An entry into to the world of spacecraft trajectory design and optimization. The problem statement is to capture two planetary systems with one launch from earth, which means the initial part of the trajectory of a spacecraft which separates into two has to be the same. After separation, one half of the spacecraft will capture Saturn after takin…

Spacecraft Guidance and Navigation Assignments from Politecnico Di Milano 2022

Full-ephemeris dynamics integration in Julia

Simulate the orbital motion for a CubeSat (HokieNav) as part of a senior design project with VT's ECE department sponsored by The Aerospace Corporation.