Full-ephemeris dynamics integration in Julia
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Updated
Jun 12, 2024 - Jupyter Notebook
Full-ephemeris dynamics integration in Julia
My quest to learn JAX and make an autograd implementation of the Q-Law
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.
Solar sailing, slightly speedier.
Solar Lyapunov Guidance Algorithm
space debris re-entty calc
Spacecraft Guidance and Navigation Assignments from Politecnico Di Milano 2022
Software development and engineering project for solving the spacecraft-moon-Earth three-body problem.
Trajectory optimization tools for lunar missions
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…
Designing an interplanetary trajectory to planet Mars 🌕
A tool for planning flights from one celestial body in KSP to another
A library to track spacecraft, written in C/C++
Fast, accessible, accurate orbit propagator for spacecraft
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.
ParaView template project for orbital data visualization (orbits, trajectory points, ground station field of view)
Spacecraft atmospheric entry simulations using Python
A proof-of-concept for building Orbiter spaceflight simulator addons in Rust
Multi-rendezvous Spacecraft Trajectory Optimization with Beam P-ACO
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