AEROX
AEROSPACE SYSTEMS PORTFOLIO
INITIALIZING... 0%
STANDBY
ALT0 km
VEL0 m/s
THROTTLE0%
FUEL100%
MISSIONSTS-001
STATUSNOMINAL
SCROLL TO LAUNCH
AEROSPACE ENGINEER & SYSTEMS ARCHITECT

BEYOND
THE EXOSPHERE

Designing the systems that carry humanity to orbit and beyond — from ignition to insertion.

T−10
MAIN ENGINE START SEQUENCE
LIFTOFF
WE HAVE LIFTOFF OF THE SPACE SHUTTLE

Emanuele
Magno

Aerospace engineering student and aspiring GNC engineer focused on spacecraft simulation, orbital dynamics, and control systems. Passionate about combining physics-based modeling with software development to build realistic aerospace simulations and interactive 3D systems.

5+
PROJECTS
GNC
FOCUS AREA
AMBITION
GNC
95%
Orbital Mechanics
92%
Propulsion Systems
88%
CFD / FEM Analysis
85%
Software (Python/C++)
93%
MAX-Q
MAXIMUM DYNAMIC PRESSURE
ALTITUDE: 14 km — MACH 1.7

Selected Projects

GNC
2026-04-04 09:11:22.076016+00:00 FINISHED

Astra GNC

ASTRA GNC is an advanced simulation framework designed to model and analyze Guidance, Navigation, and Control (GNC) systems in realistic aerospace scenarios. The project integrates physical models and numerical algorithms to simulate the dynamic behavior of spacecraft, enabling the study of orbital trajectories, propulsion maneuvers, and attitude control systems.

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Aerospace Simulations and Projects Python MATLAB 3D Modelling and Printing
GNC
2026-04-12 10:47:06.350070+00:00 Deployed

Satellite ADCS

This script is used for testing a LEO satellite GNC and orbital dynamics simulation in MATLAB. It imports Simulink outputs (position, attitude, angular rate), builds a Satellite Scenario, and visualizes orbit, attitude, and basic performance metrics (altitude, inclination, angular velocity) for validation purposes.

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Aerospace Simulations and Projects MATLAB
Orbital Mechanics
2026-04-13 15:45:45.727447+00:00 Deployed

Hohmann Transfer Simulation

A simple simulation which represents a Hohmann Transfer orbital manevreus.

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Aerospace Simulations and Projects MATLAB
ORBIT INSERTION
MECO — MAIN ENGINE CUTOFF
28.5° INCLINATION — 408 km APOGEE