INTEGRATOR FOR AIRCRAFT ASTATIC CONTROL SYSTEM Russian patent published in 2010 - IPC G05B13/00 

Abstract RU 2394261 C1

FIELD: instrument making.

SUBSTANCE: proposed integrator comprises integration signal generator 1, adder 2, integrating element 5 scaling amplifier 4, signal limiter 5, inverting amplifier 6, first 7 and second 12 controlled gates, first 8 and second 11 multipliers, hysteresis relay elements of negative 9 and positive 10 polarity.

EFFECT: higher dynamic accuracy.

3 dwg

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RU 2 394 261 C1

Authors

Syrov Anatolij Sergeevich

Puchkov Aleksandr Mikhajlovich

Tatsjuk Dmitrij Grigor'Evich

Krajnov Aleksandr Konstantinovich

Tarasov Vladimir Il'Ich

Kareva Elena Mikhajlovna

Dates

2010-07-10Published

2008-10-31Filed