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
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.
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.
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
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