FIELD: aircraft engineering.
SUBSTANCE: proposed system comprises automatic and manual control circuits. Automatic control circuit comprises the main and standby channels of conversions and computations including the main and standard units of conversion and computations, respectively, each being connected via bidirectional multiplex channel of data exchange with aircraft general equipment via control and switch unit. Manual control circuit is composed by the overhead panel. This system is connected with onboard complex of radio electronic hardware. Control system incorporates signal concentrator units, n-control units and switching units. Automatic circuit comprises extra control channel including control unit of computations and conversions. The main, standby and control units of computations and conversions are connected via bidirectional multiplex channel of data exchange via signal concentrators with overhead panel and, via said n-units of control and switching with aircraft general equipment actuators.
EFFECT: higher flight safety.
2 cl, 1 dwg
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Authors
Dates
2014-06-10—Published
2012-11-27—Filed