FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft control systems. Electronic system (1) for control over the flight of hovering aircraft (100) equipped with at least one screw (102, 104) can be operated in manual control mode and two automatic control modes corresponding to flight modes. In manual mode, flight control system (1) controls the screw rpm in response to direct instructions of pilot. In automatic mode, flight control system (1) performs automatic control over screw rpm on the basis of flight conditions. Said control system (1) can memorise for every automatic mode an appropriate flight table relating different screw rpm with different magnitudes of at least one flight index and automatically control screw rpm in flight automatic modes on the basis of appropriate flight tables.
EFFECT: safe automatic control over aircraft screw rpm.
11 cl, 7 dwg
