发明名称 DEVICE FOR CONTROLLING ANGULAR ORIENTATION SYSTEM OF AIRCRAFT
摘要 FIELD: aircraft engineering, in particular, systems for controlling angular orientation systems. ^ SUBSTANCE: device has sensors of banking angle, course, pitch and angular speeds of course, banking, pitch, three differentiation blocks, connected to appropriate angular speed indicators, subtracter, first input of which is connected to angular speed indicator of banking, and second one is connected to output of appropriate differentiating block, subtracter output, and also outputs of angular speed indicators for course, pitch and outputs of two other differentiating blocks are connected to existing squarers, and outputs of squarers respectively to adding, subtracting, adding, subtracting, adding inputs of adder, output of which is connected to first input of comparator, second input is supporting, output of which is output of device. ^ EFFECT: higher reliability of angular orientation system and higher control trustworthiness. ^ 1 dwg
申请公布号 RU2265876(C1) 申请公布日期 2005.12.10
申请号 RU20040115430 申请日期 2004.05.21
申请人 发明人 CHERNOV V.JU.
分类号 G05B23/02 主分类号 G05B23/02
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