About the Algorithm for Setting up the Control Scheme for Hybrid Unmanned Aerial Vehicles

An approach to the control law synthesis of complex unmanned aerial vehicles based on the known control of aerial vehicles with the same mass and inertial characteristics is proposed. For a “complex” UAV, a vehicle that is close in flight mechanics and relatively simple is selected according to the scheme for creating the forces and moments required for control. The parameters of PID controllers for UAV controlling of a more complex design are determined from solving a regression problem using the least squares method when simulating a flight along a program trajectory. Theoretical studies are supported by computational and natural experiments demonstrating the performance of the proposed method.