Designing the systems that carry humanity to orbit and beyond — from ignition to insertion.
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.
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.
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.
A simple simulation which represents a Hohmann Transfer orbital manevreus.
MATLAB/Simulink aerospace simulation of a spacecraft (the space shuttle) in orbit which attitude in the form of quaternion is controlled and carried out.
In this project is simulated the launch of the space shuttle using matlab and simulink combined with aerospace tools.
A simulation in which is visualized in Kerbal Space Program the entire space flight of a spacecraft using a MATLAB/Simulink model.