GEONMI-MEMS-VLEO-Engine2

GEONMI-MEMS Engine

Project Status: Proprietary Architecture Core Language: C++17 Domain: VLEO Spacecraft Dynamics Author: Mohamed Talal Kadri Contact: Email Image Image

https://github.com/user-attachments/assets/d9a2f3f4-e629-4b33-9e55-1d105eff86f6

🌐 Civil Compliance & Eco-Friendly Design Notice

The GEONMI-MEMS engine is designed, developed, and maintained strictly as a green, eco-friendly, and civil-use technology optimized for climate intelligence, ozone tracking, and space debris monitoring. This framework does not incorporate military-grade specifications, nor is it engineered for defense-classified applications. By prioritizing sustainable orbit life management and eco-friendly mission profiles, intellectual property transfers and technology licensing remain fully aligned with global civil space compliance and environmental sustainability standards.

A Closed-Loop Autonomous Dynamics & Micro-Propulsion Engine for Next-Generation VLEO Constellations.


🔒 Confidentiality Notice & Repository Status

IMPORTANT: The core source code, low-level architecture implementations, and hardware integration scripts of the GEONMI-MEMS engine are strictly proprietary and closed-source. They are securely maintained in a separate, private repository to ensure complete confidentiality and absolute intellectual property protection. Only high-level overviews and validation dashboards are showcased publicly.


🔴 LIVE HIL REAL HARDWARE - Mission Control Dashboard

GEONMI-MEMS-VLEO-Engine2 HIL Dashboard

**GEONMI-MEMS-VLEO-Engine2 SERIAL: /dev/ttyACM0 ● CONNECTED BAUD: 115200 MODE: HIL REAL HARDWARE**
ALT: 250km | LIVE 100Hz | PID: LOCKED | ZERO-HEAP: PASS      

Executive Overview

GEONMI-MEMS is an advanced aerospace computing engine engineered to address the critical flight dynamics and control challenges of Very Low Earth Orbit (VLEO ~250 km) satellite constellations. By integrating atmospheric drag compensation, closed-loop micro-propulsion thrust modeling, and resilient state estimation for GNSS-denied environments, GEONMI-MEMS provides a comprehensive architecture for constellation station-keeping, precision orbit propagation, and secure satellite-to-satellite link operations.


🛰️ LIVE Orbit Visualization - VLEO 250km

SATELLITE SIM DASHBOARD v2.4.1

SAT-ID: GEONMI-VLEO-01 | INCLINATION: 97.4° | ORBIT: VLEO | TLE REFRESHED

Interactive Demo: Open GEONMI-MEMS-VLEO-Sim.html in your browser for real-time 3D simulation.


📊 Simulation Outputs & Validation Results

GEONMI Closed-Loop Results Closed-Loop Validation @ VLEO 250km | NRLMSISE-00 Atmospheric Model | GNSS-Denied

The integrated HTML simulation validates the core claims under real-time constraints:

Parameter Simulated Output Status
Orbital Altitude 250 km VLEO Locked
Atmospheric Drag 0.23 mN (NRLMSISE-00) Estimated
Micro-Thrust 0.23 mN ±0.001 mN Compensating
Control Loop 100Hz Deterministic PID LOCKED
State Estimation GNSS-Denied Active Resilient
Memory Model Zero-Heap Allocation PASS

Note: This chart represents high-level mission outputs and telemetry results only. Core proprietary algorithms and hardware schematics remain private under Proprietary IP and are shared under NDA only.


🛠️ Core Engineering Features


🔒 Intellectual Property & Official Warning Notice

Official Warning: All rights reserved © 2026 Mohamed Talal Kadri. The GEONMI-MEMS engine architecture, source code, algorithms, hardware schematics, and associated documentation are proprietary intellectual property. Unauthorized copying, distribution, modification, reverse engineering, or commercial exploitation of any part of this project—in whole or in part—is strictly prohibited without prior written consent and a formal Non-Disclosure Agreement (NDA) with the owner. Legal action will be pursued against any unauthorized use or infringement.