FIELD: physics; control.
SUBSTANCE: invention relates to automated control systems for technological processes during ground testing of space-rocket equipment and can be used in developmental testing of aviation and transportation equipment, as well as chemical plants. The technical result is achieved through the apparatus for synchronising the control system for stand tests of space-rocket equipment and includes, in the processor of each master controller, a unit for interfacing with a local area network, connected through a control unit to a cycle counter, a cycle duration timer, a transportation delay register and a correction period counter, connected to a correction time register.
EFFECT: providing universal time and synchronisation of operating cycles of a distributed network of homogeneous master controllers irrespective of their number, arrangement and back-up version.
1 dwg
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