Python simulation of CubeSat attitude control using pyramid-configured reaction wheels. Features quaternion-based cascaded controller, wheel saturation logic, fault tolerance, and real-time 3D animation. Modular architecture for easy customization and learning.
Energy-Aware Holistic Optimization in UAV-Assisted Fog Computing: Attitude, Trajectory, and Task Assignment
This is the main repository for the codes for Spacecraft Attitude Control course Final Project - Politecnico di Milano
🛰️ MATLAB simulator for pure magnetic detumbling of fast-tumbling picosatellites: B-dot control, IGRF environment, realistic magnetorquers and magnetometers, and Monte Carlo campaigns. Code behind the IAC-18 paper.
Application of kynodynamical motion planning algorithms to perform attitude maneuvers for a magnetorquer-actuated LEO satellite with pointing constrains.
C++98 modular simulator for attitude control of a 3D rigid body. Implements physical dynamics, PID-based feedback control, sensor emulation with noise and drift, and delayed actuator execution. Designed with testability, precision, and embedded system constraints in mind.
Fault-tolerant GNC avionics suite for bench-top model rocketry — attitude estimation, closed-loop control, and bidirectional ground station on Raspberry Pi 5
Research and development (R&D) refers to the set of activities companies undertake to innovate and introduce new products and services.
An example of user settings repository for c2a-aobc
Physics-based quadcopter simulation with rigid-body dynamics and cascaded PD attitude control, serving as a foundation for constrained and optimization-based control methods.
Visualize and debug quaternions
An example of user settings repository for s2e-aobc
Hybrid AI-Powered Satellite Attitude Determination and Control System (ADCS) integrating MEKF, quaternion dynamics, LQR/PD control, and neural network-based attitude control for spacecraft GNC applications.
Research project where was developed a new Guidance, Navigation and Control (GNC) law for Attitude Determination and Control Systems (ADCS) of CubeSat satellites.
6-DOF spacecraft attitude dynamics and control simulation for a Mars nanosatellite with autonomous mode switching
To determine the physical parameters, model and mathematical representation of a magnetorquer.
Lateral flight controller design for a B-747 using classical control(lead/lag compensator & wash-out filter) and LQR
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