Aircraft overload flight control

The article discusses the issue of changing the spatial position of the center of mass of an aircraft by controlling overloads through appropriate channels. The object is described by a system of equations of motion of an aircraft expressed for overloads in the state space. Examples of the implementation of equations of the control object model, as well as models of the overload control system in the MATLAB Simulink mathematical modeling environment are given. The coefficients of the regulator for each channel of the control system are determined. Graphs of changes in the coordinates of the center of mass of the product through the control channels are constructed, as well as graphs of changes in current overloads during the maneuver. Conclusions are drawn about the quality of the processes provided by the control system, as well as about the safety for humans on board the aircraft.