FIELD: transport.
SUBSTANCE: electronic control device for aircraft flight control component including flight controlled element. The latter is connected with one or more aircraft control component. Flight control element is fitted at electromechanical case with at least one degree of freedom. Said electromechanical case comprises one or more motors and motor position transducers. Electronic control device comprises command-and-control module of flight controlled element, The latter comprises one or more electronic microcontroller. The latter generates control signals for controlled element drive motors and receive signals from transducers. It effects digital processing of signals from transducers connected with one second degree of freedom of the first control component and generates signals in the case of faults.
EFFECT: higher safety and reliability.
13 cl, 2 tbl, 11 dwg
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Authors
Dates
2015-01-10—Published
2010-11-01—Filed