GAAS is an open-source program designed for fully autonomous VTOL(a.k.a flying cars) and drones. GAAS stands for Generalized Autonomy Aviation System.

Teensy/Arduino flight controller and stabilization for small-scale VTOL vehicles

Curated list of free software and hardware to build remote controlled copters and planes

An interactional aerodynamics and acoustics solver for multirotor aircraft and wind energy

Flight Controller for ESP32 / Raspberry Pico / STM32

Library for Aircraft Dynamics And Control

NextPilot Flight Control System is a powerfull, scalable and advanced autopilot, which is designed to be easily used in education, research, and industry.

Full dynamic model for the Babyshark 260 VTOL UAV.

Examples for the Library for Aircraft Dynamics And Control

This repository contains the VTOL book latex source, as well as simulation code.

A fork (copy) of AirSim's Unreal Engine Plugin with added functionality for VTOL aircraft.

This project is used to estimate, isolate and diagnose faults for a quadcopter and a PVTOL and also use a methods to control the system by tolerating the fault. Both quadcopter and PVTOL systems have nonlinear dynamics. The ways for fault estimation in this project consist of nonlinear AO and linear PIO for the PVTOL and qLPV PIO for the quadcop…

PX4 VTOL off-board control in ROS2 for autonomous agile flight

fatqat is a ground control station software with image processing apps for ArduPilot systems.

Single Rotor VTOL UAV

Preliminary design optimization for a tiltrotor drone under 25kg and slower than 45m/s

A tutorial on using and extending VTOL-AirSim.

One degree-of-freedom (1 DOF) Vertical Take-Off and Landing (VTOL) benchmark using the ESP32 for data acquisition and LabVIEW for PID control and response visualisation.

This toolbox is to ease the process of finding design parameters for fixed-wing battery-powered vertical take-off and landing drones. The toolbox will be regularly expanded to include more variations and design considerations.

Control algorithms and code pertaining to the thrust vector control