The Control platform program will be based on applied methods of synergetic synthesis of nonlinear control systems for unmanned aerial vehicles, allowing for the creation of positional and trajectory control regulators that take into account the internal dynamics of the drive system, which will improve the efficiency of control and ensure greater flight stability and sustainability. The protection mechanisms built into the design and implementation stage of the Control platform allow for increased reliability and fault tolerance of the development, as well as protection against unauthorized access to critical information, even if the device is intercepted by an intruder. Design of a modular architecture of a flight controller to ensure easy expansion of the flight controller functionality and adaptation of the design to new components. Development of a flight controller design based on the method of analytical design of aggregated discrete regulators of synergetic control theory. Design of a control board based on a modular approach with the possibility of adaptation and optimization methods to ensure the possibility of replacing components. Development of modules according to the established standards of the main board, selection of components to create an optimal copy of the product.