Porkchop plot tool for interplanetary transfer analysis.
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Updated
Jul 15, 2024 - Python
Porkchop plot tool for interplanetary transfer analysis.
GNC toolkit with python
A tool to build porkchop plots with Rust 1.96 and Python 3.14
Pork-Chop plot for Lambert's Problem of a Earth-Mars mission
Numba port of pykep's Izzo Lambert solver for parallel transfer tables, benchmarked against pykep and pykep-rust (ESA SpOC 4, 12.9x faster table build).
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.
Pure-Rust astrodynamics ported from pykep 3: Lambert, Kepler/Taylor propagation, Sims-Flanagan, low-thrust and MGA trajectory problems; Python wheel pykep-rust.
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.
Independent check of the hapsira, Orekit and Basilisk orbit propagators and Lambert solvers against closed-form references.
Venus–Mars–asteroid transfer design and J2/SRP perturbation analysis around Venus, in MATLAB
An audit of 17 starred space and optimisation repositories against the economicspace asteroid-mining pipeline: dated findings, read-only delta-v and taxonomy probes, and the licence record of what was taken from each
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.
Learning Julia through orbital mechanics: element conversions, propagation, Hohmann and Lambert transfers
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