FIELD: missilery.
SUBSTANCE: invention is related to the field of aviation controlled missiles. Substance of invention consists in preparation of missile on board of carrier airplane for work, measurement of target movement parameters and missile own movement, generation of assessment of necessary parameters of target relative movement and missile absolute movement, selection of method of missile homing at target of the best application by any criterion for these conditions. Parameters of mismatch are calculated for selected method, the said parameters characterising extent of mismatch of actual parameters of missile movement and their required values. Analysis of jamming environment is carried out, noise protective facilities and non-radio-radar meters being switched on depending on jamming environment. Formation of preparation and control signal is carried out for radio proximity fuse. Based on current values, angle position and target range rate of missile approaching target is determined, as well as module of missile miss, geometric dimensions and target angle. On the basis of these data commands are generated for blasting of missile warhead and for initial speed of missile warhead fragments emission.
EFFECT: increased efficiency of operational use.
21 cl, 13 dwg
