SPACECRAFT ATTITUDE CONTROL SYSTEM Russian patent published in 2006 - IPC B64G1/26

Abstract SU 1839997 A1

FIELD: space engineering.

SUBSTANCE: proposed system is provided with orientation sensor, amplifier-adder, correcting unit with differential gear and time-delay unit connected in series, logic gates, actuating member with built-in tachogenerator and normally open switch. Memory is connected between switch and amplifier-adder.

EFFECT: enhanced accuracy.

2 dwg

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SU 1 839 997 A1

Authors

Golubev Petr Vasil'Evich

Karpenko Veniamin Maksimovich

Frolov Vadim Petrovich

Dates

2006-06-27—Published

1970-09-11—Filed