| 摘要 |
PURPOSE: To control a flying angle and timing by matching the directivity of a warhead to a target and selecting a detonation point to achieve an attack according to the target, generating a detonation signal by an electrical fuse in the output signal of a bullet piece scattering range calculation device for igniting a bursting charge for detonation from a local part using a microprocessor. CONSTITUTION: When a target 16 approaches a missile at a certain speed and a distance R between targets, a calculation device 11 of the missile calculates the speed of the target, obtains a bullet piece scattering distance R1 from the value of a distance R13 between targets being obtained by measuring distance by a proximity fuse 24 and a warhead scattering angleθ, calculates a bullet piece speed, target time when a bullet piece travels the distance R between targets, the relative speed of the missile, and a target traveling distance R2 (R2 is variable) from time immediately after passing a point (b), and sends the values of R1 , R2 , and R3 to a microprocessor 1. A microprocessor 12 selects a detonation point for a direction for detecting a target according to a side antenna pattern. When a detonation signal is inputted from the proximity fuse 24, it is outputted to an electrical fuse 6, and the electrical fuse 6 ignites detonation power 8 through a transfer mechanism 7 and ignites bursting charge 4 from a local part.
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