FIELD: transport.
SUBSTANCE: invention relates to aerospace engineering and may be used in spacecraft onboard control systems. Proposed system comprises three control channels. Every said control channel comprises control signal setting device, angular velocity transducer, unit of intermittent switching, switch, unit of jet engines, angle transducer, comparator, adding amplifier and relay element connected in series. Comparator is connected with control signal setting device, adding amplifier is connected with angular velocity transducer, and intermittent switching unit is connected with switch.
EFFECT: lower power consumption, decreased weight, minimised quantity of jet engines.
4 dwg
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