| 摘要 |
FIELD: weapons and ammunition. ^ SUBSTANCE: group of inventions is related to the field of aviation controlled rockets. According to method for functioning of information-computing system of rocket, they perform narrow-band beam scanning of electromagnet oscillations in sector specified relative to rocket axis, then frequency bands that correspond to frequencies of air target power plant vibrations are separated from spectrum reflected from extended target of signal. Maximum value of vibration amplitude is defined in specified band of frequencies of reflected signal spectrum from extended target, values of current and maximum amplitude of vibrations are compared in each angular position of antenna with further scanning of extended air target, angular position is defined for power plant of air target at the moment of equality of current and maximum value of reflected signal vibration amplitude. Rocket is re-aimed at power plant of air extended target, radiation and reception of electromagnet vibrations is carried out by means of narrow beam scanning in specified sector relative to rocket axis as rocket approaches the second specified distance, frequency bands that correspond to frequencies of target structure elements vibrations are separated from spectrum of signal reflected from target, values of reflected signal maximum amplitude are defined in this frequency band, radiation and reception of electromagnet oscillations is fixed in direction specified relative to axis of rocket, target structure element having maximum vibration amplitude is recognised, and signal is generated for explosion of rocket warhead during combination of fixed beam of electromagnet vibrations with this element of structure. Device is developed for method realisation. ^ EFFECT: higher efficiency of war using of the rocket. ^ 8 cl, 3 dwg |
