FIELD: physics.
SUBSTANCE: invention relates to aircraft control systems and is intended to provide operation of trimmer effect mechanism (TEM) at interaction of manual and automatic control.
EFFECT: invention improves reliability of trimmer effect of manoeuvrable aircraft due to longer service life due to reduced switching frequency of actuating electric motor, to ensure stable operation when operating in follow-up circuit with simultaneous provision of acceptable accuracy characteristics.
1 cl, 4 dwg
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Authors
Dates
2020-04-21—Published
2018-12-25—Filed