CONTROL SYSTEM OF SPACECRAFT Russian patent published in 2018 - IPC G06F11/07 G05B15/02

Abstract RU 2653243 C1

FIELD: electrical engineering.

SUBSTANCE: invention relates to electrical engineering and can be used in autonomous power systems for space vehicles, as well as in other devices requiring high reliability. For this purpose, a control system for the instruments of the spacecraft is proposed, which includes three computational complexes (CC), a driver of reconfiguration commands (DRC), the majority elements (ME, additionally contains three registers with Z-state, and between each two inputs of each ME a resistor ME is installed. DRC is made in the form of a restartable monostable, and the power outputs of the DRC, registers and each CC are designed to be connected to an independent power source.

EFFECT: technical result is an increase in reliability and a decrease in the mass of the spacecraft.

3 cl, 3 dwg

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RU 2 653 243 C1

Authors

Varenbud Leonid Ruvimovich

Tishchenko Artem Olegovich

Shatalov Igor Mikhajlovich

Dates

2018-05-07—Published

2017-05-18—Filed