A project to calibrate the BNO055 IMU from Bosch and Adafruit for CubeSat Satellite GNC.
3D missile guidance simulation — PN, APN, OGL with seeker, filter, autopilot dynamics, and Monte Carlo analysis
A user-friendly toolkit for engineers and researchers to address the problem of aligning measurements from gyroscopes mounted on the same rigid body.
A flight-ready satellite mission control system built on real orbital physics, autonomous GNC, and AI-driven trajectory optimization. CommandX brings together the tools mission operators need — from live fleet monitoring to hardware stress simulation — inside a single command interface.
6-DOF fixed-wing UAV simulation with cascaded PID autopilot, cross-track guidance, Dryden turbulence (MIL-HDBK-1797), and an EKF for IMU/GPS navigation.
Project to design a test platform to suspend a satellite, for recreating the low-friction conditions they are subjected in space and to test ADCS performance of CubeSat.
High-fidelity CubeSat OBC Flight Software in C with Virtual Hardware-in-the-Loop (vHIL) simulation.
This is a Python package for getting easy access to tools needed to perform calculations and transformation related to guidance, navigation and control (GNC) tasks. It is based on the tools used in PythonVehicleSimulator and MSS Toolbox by Thor I. Fossen.
This project is about the determination and simulation of enviromental disturbances for a 1U CubeSat.
Research project where was developed a new Guidance, Navigation and Control (GNC) law for Attitude Determination and Control Systems (ADCS) of CubeSat satellites.
To determine the physical parameters, model and mathematical representation of a magnetorquer.
Mission-control telemetry simulation and anomaly surfacing stack for orbital monitoring and operator-facing dashboards.
Controls and simulation project to balance an inverted pendulum
A lightweight Python toolkit for early-stage parafoil design, sizing, and trajectory simulation using low-fidelity aerodynamic models.
This repository provides a high-fidelity framework for space mission design, focusing on CRTBP dynamics, low-thrust trajectory optimization, and non-linear uncertainty propagation. It features advanced GNC tools, including Unscented Kalman Filtering and Batch Orbit Determination validated with ESA mission data.
End-to-end simulation of a guided 155mm Ramjet projectile. Integrates high-fidelity ANSYS Fluent CFD (Mach 2.0) with a custom Python 6-DOF flight dynamics engine and Proportional Navigation (PN) control loop for precision target intercept.
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