发明名称 ADAPTIVE INTEGRAL DEVICE FOR SYSTEMS OF AIRCRAFTS CONTROL
摘要 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
申请公布号 RU2393521(C1) 申请公布日期 2010.06.27
申请号 RU20080143095 申请日期 2008.10.31
申请人 FEDERAL'NOE GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE MOSKOVSKOE OPYTNO-KONSTRUKTORSKOE BJURO "MARS" (FGUP MOKB "MARS") 发明人 SYROV ANATOLIJ SERGEEVICH;PUCHKOV ALEKSANDR MIKHAJLOVICH;KRAJNOV ALEKSANDR KONSTANTINOVICH;CHEREPANOVA VALENTINA EVGEN'EVNA;ZHDANOVICH NADEZHDA PAVLOVNA
分类号 G05B13/00 主分类号 G05B13/00
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