Control System Design of a H-shape configuration Fixed Wing VTOL based on a Patented Vertical Thrust System

The study is dedicated to design a control architecture for a Lift+Cruise aircraft utilizing the patented ThrustPod technology. This innovative approach integrates Fixed Wing functionalities with retractable rotors to facilitate Vertical Take-Off and Landing. By transitioning between Multirotor and Fixed Wing modes, it enhances aerodynamic efficiency while preserving vertical flight capabilities. Using Incremental Nonlinear Dynamic Inversion, the control system autonomously manages each flight phase, supported by a state machine framework for mode transitioning. Through simulations based on realistic mission scenarios in mountain areas, the system demonstrates reliable performance across various flight regimes. The proposed integrated solution represents progress in Urban Air Mobility, potentially offering a practical transportation option for passengers and cargo in challenging environments.