Analytical Design of the Law for Control of the Center of Mass Motion for an Unmanned Aerial Vehicle

The control of the lift direction in space is considered. We synthesized the control of the mechanism of the center of mass motion in the longitudinal direction for regulating the static margin and in the transverse direction for creating the balancing equilibrium at the angle of attack and air-path bank angle. The structure of the law to control the angular acceleration is chosen, formulas to calculate the control parameters are obtained.