mission-design

Satellite Mission Analysis and Design based on Orekit

Low-thrust mission design for asteroid mining and beyond: which targets a spacecraft can reach, sizing the spacecraft to get there, and planning the trajectory to fly.

e2m2e 是地月空间算法工具集。

Trajectory optimization framework that uses indirect methods

B2XKlaim: a BPMN-to-X-Klaim toolchain for model-driven multi-robot mission design.

A modular, professional-grade digital engineering and trajectory propagation platform for spacecraft propulsion systems. Includes high-fidelity physics models (Hall effect, gridded ion, chemical, nuclear, and VASIMR engines), multi-node thermal LPN solvers, power simulation, state estimation (EKF), and automated engineering advisor analytics.

Satellite tracking and manoeuvre detection from public orbital data

Preliminary Design Of The Trajectory For An Interplanetary Mission Between Earth And Saturn With Natural Gravitatory Assistance From Jupiter

80 validated aerospace-engineering tools for Python, the CLI, and MCP agents: structures, aerodynamics, compressible flow, propulsion, orbital mechanics, ascent and recovery, optimization, and reliability. Every result is traceable to a published reference.

Cited reference tables for space-mission cost and mass estimation: launch vehicles, propellants with derived tankage, delta-v segments, operational costs, and storage systems. EconomicSpace subrepo

Aerospace Engineering Portfolio - GNC Systems, Mission Analysis, and Space Systems Design

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.

Natural-language to validated GMAT .script — RAG-grounded generation, lint-checked against gmat-script, with a model-agnostic CLI.

Delta-v planner for circular-to-circular transfers (Hohmann, bi-elliptic, plane-change). Impulsive burns, quick trade-offs. Python 3.10+.

Earth-Ceres mission design and upper-stage propulsion study

Backend physics engine of my space mission design tool, including trajectory design, spacecraft configuration, mission validation and payload constraint validation. Topics

EMTG Community Edition: NASA's mission trajectory design foundation with IPOPT, simpler builds, and Python interfaces for analysis and automation.

Educational Moon/Mars mission-design game with spacecraft trade-offs, deterministic simulation, an offline assistant and NASA/JPL reference data.

High-fidelity illumination modeling and N-body trajectory optimization for Enceladus mission design. Developed in MATLAB for the ESA-funded GIGANTES project.