FIELD: instrument making.
SUBSTANCE: device comprises setter of integration signal (1), summator (2), integrating link (3), scaling amplifier (4), limiter of signal (5), inverting amplifier (6), the first (7) and second (12) controlled switches, the first (8) and second (11) multiplication units, hysteresis relay elements of negative (9) and positive (10) polarity, sensor of speed discharge (13), functional converter (14) and inverter (15).
EFFECT: improved dynamic accuracy in control of non-stationary aircraft with working of sign-alternating input actions.
3 dwg
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