FIELD: aviation.
SUBSTANCE: helicopter remote control system contains two control stations with control elements and stick transducers (ST), four drive control units (DCU), two integrated sensor units (ISU), two signal transformation units (STU), a reserve navigation unit (RNU), four electromechanical drives, a standby channel signal quorum unit (SQU), an architecture control unit (ACU), two computing devices (CD), and an onboard equipment complex (OEC) connected in a certain way.
EFFECT: increased reliability of the remote control system by enabling equipment reconfiguration.
1 dwg
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