Porkchop plot tool for interplanetary transfer analysis.
Pork-Chop plot for Lambert's Problem of a Earth-Mars mission
A tool to build porkchop plots with Rust 1.96 and Python 3.14
GNC toolkit with python
This folder contains script to solve the MRPLP using Differential Algebra techniques
University project developed as part of the final coursework requirements for Aerospace Engineering at Politecnico di Milano. This work was not formally published by Politecnico di Milano.
A Rust implementation of Lambert’s Problem for computing orbital transfer velocities between two position vectors given a time of flight.
Interplanetary trajectory planner: solves Lambert's problem with real ephemeris data to compute optimal Earth-Mars transfer windows, generates porkchop plots, and animates the mission in interactive 3D.
Analysis and optimization of an interplanetary mission which consisted in a transfer from Saturn to an asteroid through a flyby with Jupiter, study of a planetary explorer mission for Earth observation
Patched-conic Earth-Mars transfer window: analytic ephemerides, Lambert targeting, porkchop sweep, independent validation. Final selected transfer: 2026-10-31 -> 2027-09-07, C3=9.23 km^2/s^2, dv=5.68 km/s.
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