DEVICE FOR CONTROL OF SPINNING MISSILE Russian patent published in 2006 - IPC B64C13/18 

Abstract SU 1839988 A1

FIELD: aeronautical engineering.

SUBSTANCE: proposed device has command signal shaping unit, reference voltage generation unit, modulator and servo unit connected in series. Device is also provided with multiplier unit whose first input is connected with output of modulator and second input is connected with output of reference voltage generation unit; device is also provided with aperiodic filter and adder whose second input is connected to output of command signal shaping unit and its output is connected to modulator input.

EFFECT: enhanced dynamic accuracy.

1 dwg

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SU 1 839 988 A1

Authors

Zhuravlev Sergej Dmitrievich

Morozov Vladimir Ivanovich

Parfenov Jurij Leonidovich

Kuznetsov Jurij Matveevich

Dates

2006-06-20Published

1984-11-14Filed