Tools for professional robotic development in C++ and Python with a touch of autonomous driving and aerospace

Portable reference implementation of the UAVCAN protocol stack in C++ for embedded systems and Linux.

PyKEP is a scientific library providing basic tools for research in interplanetary trajectory design.

An Aircraft Design Toolbox

Aircraft design optimization made fast through modern automatic differentiation. Written in Python, work in progress.

A compact implementation of the UAVCAN/CAN protocol in C11 for high-integrity real-time embedded systems

Hypersonic / Rarefied gas dynamics code developments (GPL-3.0)

Python implementation of the UAVCAN protocol stack.

Matlab implementation to simulate the non-linear dynamics of a fixed-wing unmanned areal glider. Includes tools to calculate aerodynamic coefficients using a vortex lattice method implementation, and to extract longitudinal and lateral linear systems around the trimmed gliding state.

no std uavcan lib in rust. For embedded and general software.

A curated list of aerospace/space related data and code resources for a community of independent hackers dedicated to furthering humanity's knowledge of the universe through open collaboration.

a mechanical engineering toolbox

The UAVCAN specification documents are maintained here.

Distributed, workflow-driven integration environment

The minimum viable release of the Ptera Software Suite: a fast, easy-to-use, and opensource software package for analyzing flapping-wing flight.

Regulated DSDL definitions for UAVCAN (standard and third-party)

Machine Learning + Spacecraft Trajectory Optimisation

Demo for analyzing the structural imbalance on a signed social network.

Incorporating Inductive Bias into Deep Learning: A Perspective from Automated Visual Inspection in Aircraft Maintenance

Resources for analyzing aircraft structures for aerospace engineers

An autonomous Thrust Vector Control rocket with self-landing capability from inexpensive parts of equivalent power of the Apollo era.

Computational Aerodynamics Lab

Legacy website, now obsolete.

This project outputs G-code that is used to control a 4-axis hot wire cutter, employed to cut a wing / airfoil from a physical block of foam. Effectively, it is a slicer for a particular arrangement of raw-coordinate data files.

Group satellites into constellations such that their average observation coverage is maximized

Structural analysis of the aileron of a Boeing 737

Demonstration of Conventional 2 Sensor Attitude Determination using VRML in Simulink

SpaceLab Organization Info

Download satellite orbital elements from Space Track and other sources

GranaSAT Ground Station Control Dashboard