The guidance algorithm of air-to-air guided missile with an active radar target-seeking head to a helicopter with various modes of its flight

On the basis of the mathematical apparatus of the statistical theory of optimal control, the method and algorithm of guidance of an air-to-air guided missile with an active radar target-seeking head when aiming at a «helicopter» class air target with various modes of its flight, including when hovering have been developed. The synthesis has been carried out as a result of flight experimental studies of radar signals reflected from a real helicopter. Also, recommendations for ensuring continuous tracking of a helicopter in an active radar target-seeking head have been presented.