FIELD: physics; computer engineering.
SUBSTANCE: invention relates to information and measuring systems and is meant for checking electrical and information interaction of a rocket with carrier equipment using a device which simulates prelaunch functions of a rocket. The said simulation device has several independent channels and can simulate several rockets for simultaneous control of several suspension points and realising a simultaneous start mode. Each channel includes one-time command input-output lines and digital data input-output lines. The simulation device has a control module in form of a processor board, a digital data input-output module, a one-time command input-output module, a digital data error assignment module, a one-time command error assignment module, an information display module, an information exchange assignment module, and at least one channel which has an input-output socket.
EFFECT: more reliable simulation of electrical and information interaction of a rocket with carrier equipment.
10 cl, 3 dwg
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Authors
Dates
2009-12-27—Published
2008-01-29—Filed