| 摘要 |
FIELD: missile control systems. SUBSTANCE: first claim of invention describes design of device which has unit for generation of guidance commands, missile rotation detector, which is connected to gyro, two comparators, power amplifier which is connected to missile control drive, two controlled clippers, two absolute value calculation units, XOR gate. Another claim of invention describes design of device which has unit for generation of guidance commands, missile rotation detector, which is connected to gyro, two comparators, power amplifier which is connected to missile control drive, two controlled clippers, two absolute value calculation units, clipper and XOR gate. EFFECT: decreased distortions in control process. 2 cl, 7 dwg
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