METHOD OF DATA COMPUTING SYSTEM OPERATION OF MISSILE AND DEVICE FOR ITS IMPLEMENTATION Russian patent published in 2008 - IPC B64D7/00 F41G3/22 F41G7/22 F42B15/01 

FIELD: engines and pumps.

SUBSTANCE: essence of the invention comprises in preparing a missile on board launcher-aircraft to an autonomous operation by means of a voltage supply from apparatus of a fighter, also by means of measurement of a target and missile movement parameters, by means of evaluating assessment of required parameters of a relative target and absolute missile movements, by means of a choice of aiming the missile based on the best of one of the criteria under given conditions of application, of computing of mismatch parameters for the chosen method, characterizing the degree of mismatch between actual parameters of missile movement and their required values, of generating a signal for preparation and control of radio proximity fuse. Also emanation and reception of the electromagnetic oscillations are achieved by means of a narrow band scanning in a specified sector against the axis of a missile. Upon missile approaching a target at a distance when a target is becoming dimensional, frequency bands corresponding to oscillation frequencies of target structure components are selected out of spectrum of the signal reflected from the target, then the values of maximum amplitude of the reflected signal are identified in this frequencies band. Then the emission and reception of electromagnetic oscillation in the direction specified against the axis of the missile are fixed, and the component of the target structure with maximum amplitude of vibration is recognized. At a combination of a fixed ray of electro magnetic oscillations with a given structure component a signal is generated to explode an operational portion of the missile upon receiving the signal on the target location against the missile axis and receiving the signal of identification.

EFFECT: upgrading of self-descriptiveness.

2 dwg, 7 cl