unmanned aerial vehicles; kinematic model; dynamic model; rotary-wing UAVs; fixed-wing UAVs; automatic control systems; flight stabilization; nonlinear control

The article provides an overview of modern approaches to mathematical modelling and synthesis of control systems for rotary-wing unmanned aerial vehicles (UAVs) and fixed-wing UAVs. It considers kinematic and dynamic models describing the translational and rotational motion of the mentioned types of UAVs, taking into account aerodynamic forces, moments, and gyroscopic effects.