BUILDING THE SOFTWARE AND SIMULATION
BACKBONE OF NEXT-GENERATION
FLIGHT SYSTEMS.
Guidance, navigation and control systems, high-fidelity orbital simulation and
AI knowledge graphs — bridging theoretical orbital mechanics and flight-ready software.
Design of software systems from desktop-gui to web app.
2026 — PRESENT
Independent Aerospace Engineering Projects
Developing GNC software, high-fidelity orbital simulations and optimal control systems for spacecraft and CubeSat platforms.
2026 - XXXX
Bsc Aerospace Engineering
I'm studying Aerospace Engineering on September.
01PRIME DIRECTIVES — PROJECTS
7 projects loaded from the database.
GUIDANCE & CONTROL
2026_07COMPLETED
Dual-Quaternion GNC for Interplanetary Mission
Spacecraft GNC has traditionally treated rotation and translation as separate problems: attitude is parameterized by a unit quaternion evolving under q̇ = ½ q ⊗ ω, while translation is a Cartesian vector evolving under Newton's law. For decoupled tasks this is adequate, but for coupled six-degree-of-freedom (6-DOF) maneuvers — rendezvous, proximity operations, or a thrust-vector hold in which the body pointing and the orbital position must be commanded jointly — the separation forces hand-written cross-coupling terms and duplicated bookkeeping.
PythonNumPySciPyControl
VIEW DATA →
GUIDANCE & CONTROL
2026_06COMPLETED
Dual Quaternion GNC for ISS-Class Docking
An autonomous spacecraft docking simulation implementing dual quaternion-based Guidance, Navigation and Control for precision docking with an International Space Station (ISS)-class target.
PythonNumPySciPy
VIEW DATA →
GUIDANCE & CONTROL
2026_06COMPLETED
Dual Quaternion GNC for Spacecraft Proximity Operations
A six-degree-of-freedom Guidance, Navigation and Control framework using dual quaternions to simultaneously represent spacecraft translation and rotation during autonomous proximity operations.
PythonNumPySciPy
VIEW DATA →
ATTITUDE DETERMINATION & CONTROL
2026_06COMPLETED
ADCS System – Optimal LQR Control for 3-Axis Stabilization
An optimal attitude control system that achieves precise three-axis spacecraft stabilization using Linear Quadratic Regulator (LQR) control.
PythonNumPySciPyControl
VIEW DATA →
ATTITUDE DETERMINATION & CONTROL
2026_06COMPLETED
ADCS System – Optimal LQR Control for Detumbling
An Attitude Determination and Control System (ADCS) implementing an optimal Linear Quadratic Regulator (LQR) to stabilize a tumbling spacecraft immediately after deployment.
PythonNumPySciPyControl
VIEW DATA →
GUIDANCE & CONTROL
2026_05COMPLETED
Autonomous Spacecraft GNC
A complete Guidance, Navigation and Control (GNC) simulation framework for autonomous spacecraft operations. The project integrates orbital dynamics, attitude control, trajectory guidance, and mission execution into a modular architecture designed to emulate real spacecraft autonomy.
PythonNumPyMATLAB
VIEW DATA →
SPACECRAFT SIMULATION
2026_06COMPLETED
Astra Space Simulator
A high-fidelity spacecraft simulation environment designed to visualize orbital mechanics, spacecraft dynamics, and mission operations in real time. The simulator serves as both an engineering tool and an educational platform for spacecraft system development.
PythonNumPyMatplotlib
VIEW DATA →
02KNOWLEDGE GRAPH
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03AI TERMINAL — RAG CHAT
Source: POST /api/v1/ai/conversations/chat/ — answers generated from the personal knowledge graph.
astrox@brain:~$
AstroX Brain AI Terminal initialized. Ask a question about aerospace research notes.
04PUBLIC PORTFOLIO
Profile and published items loaded from the database.
Emanuele Magno
I'm an Aerospace Engineering student, aerospace enthusiast, and software developer passionate about designing intelligent systems for space exploration.
My interests focus on Guidance, Navigation & Control (GNC), spacecraft dynamics, orbital mechanics, autonomous aerospace systems, and scientific simulation. I enjoy developing engineering software that combines physics, mathematics, and programming to solve complex aerospace challenges.
In my free time, I build aerospace simulation projects, explore advanced control algorithms, contribute to personal software projects, practice Kung Fu, fly drones for aerial photography, and continuously expand my knowledge through research and hands-on experimentation.
IMPACTOne equation to move through space. Rotation and translation, finally speaking the same language.
We didn't prove it on paper. We flew it to Duna — and held the orbit.
CV
IMPACTA step toward flight-ready software — built, tested, and proven to work, not just theorized.
IMPACTTurns raw physics into commands a real spacecraft can execute safely and precisely.
Astra Space Simulator
IMPACTLets failure happen safely on a screen instead of in orbit, before a single dollar is spent on hardware.
ADCS System – Optimal LQR Control for Detumbling
IMPACTTurns raw physics into commands a real spacecraft can execute safely and precisely.
ADCS System – Optimal LQR Control for 3-Axis Stabilization
IMPACTTurns raw physics into commands a real spacecraft can execute safely and precisely.
Dual Quaternion GNC for Spacecraft Proximity Operations
IMPACTUnifies rotation and translation in one consistent math model — fewer bugs, more reliable spacecraft motion.
Dual Quaternion GNC for ISS-Class Docking
IMPACTUnifies rotation and translation in one consistent math model — fewer bugs, more reliable spacecraft motion.
05OBSIDIAN VAULT SYNC
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EM
☍PERSONNEL FILE
EMANUELE MAGNO
DESIGNATIONAerospace Engineer & Systems Researcher
FOCUSGuidance, Navigation & Control · Orbital Simulation
Researcher focused on guidance, navigation and control, orbital mechanics simulation and
autonomous systems. My work covers trajectory optimization, real-time flight software and
high-fidelity simulation for spacecraft and CubeSat platforms. I believe in systems that behave
the same way in simulation and in flight.
GUIDANCE & CONTROL
