Pitch and Thrust Allocation for Full-Flight-Regime Control of Winged eVTOL UAVs

Trajectory tracking control for winged eVTOL aircraft is complicated by the high-angle-of-attack aerodynamics experienced during navigational flight occurring immediately after takeoff and before landing. The total energy use of vehicle can be reduced performance improved appropriately considering pitch angle in varying conditions. We present a review aerodynamic models as well an algorithm finding optimal thrust throughout its regime. show simulation results demonstrating 75% reduction error over our previous work while maintaining similar average 85% using multirotor-like controller. that method robust to modeling stall characteristics.