发明名称 METHOD OF GENERATING SIGNAL TO CONTROL AIRCRAFT ANGULAR FLIGHT AND DEVICE TO THIS END
摘要 FIELD: aircraft engineering.SUBSTANCE: control signal generator comprises control signal selector 1, comparator 2, fist amplifier 3, adder 4, filter 5, signal clipper 6, angle transducer 7, angular velocity transducer 8, second amplifier 9, velocity head transducer 10, logical comparator 11, controlled switch 12, third amplifier 13 and critical velocity head selector 14.EFFECT: expanded operating performances owing to use of velocity head parameter and higher dynamic accuracy of drone control.2 cl, 1 dwg
申请公布号 RU2490686(C1) 申请公布日期 2013.08.20
申请号 RU20120122880 申请日期 2012.06.05
申请人 FEDERAL'NOE GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "MOSKOVSKOE OPYTNO-KONSTRUKTORSKOE BJURO "MARS" (FGUP MOKB "MARS") 发明人 SYROV ANATOLIJ SERGEEVICH;ZHDANOVICH NADEZHDA PAVLOVNA;KRAVCHUK SERGEJ VALENTINOVICH;OGOL'TSOV IGOR' IVANOVICH;POPOV BORIS NIKOLAEVICH;PUCHKOV ALEKSANDR MIKHAJLOVICH;SOLOV'EV ALEKSEJ SERGEEVICH
分类号 G05D1/00 主分类号 G05D1/00
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