Development the control system algorithms functioning of flight safety for the aircraft of helicopter type

In paper the flight safety control system of the helicopter, its structure and interaction with the interfaced equipment is considered. Classification of negative situations of the onboard radio-electronic equipment of the aircraft of helicopter type is given. The algorithms allowing to execute recognition, forecasting and notification of flight crew about approach of critical control mode of the flying device are received. Distinctive feature of the offered algorithm is synthesis the methods of artificial intelligence at his realization.