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

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

SAT-ID: GEONMI-VLEO-01 | INCLINATION: 97.4° | ORBIT: VLEO | TLE REFRESHED
Interactive Demo: Open
GEONMI-MEMS-VLEO-Sim.htmlin your browser for real-time 3D simulation.
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.
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.