发明名称 CONTROL DEVICE FOR SYSTEM OF COORDINATED CONTROL OF FLIGHT VEHICLE
摘要 FIELD: control devices for on-board automatic control systems of flight vehicles with an aircraft system with realization of capabilities of regimes with coordinated turns in the side channel with large bank angles. ^ SUBSTANCE: the control device has a roll-angle pick-off, roll-rate pick-off, first and second summing amplifiers, on-course control signal setter, first and second subtraction units, non-linear component with a dead band, sign inverter, dynamic unit for matching in dynamics of on-course and bank control signals, and a non-linear component with a limiter. ^ EFFECT: attained functional potentiality of variation of the intensity (level) of control in the roll channel in the conditions of load of the yaw channel, enhanced accuracy of control. ^ 1 dwg
申请公布号 RU2237269(C1) 申请公布日期 2004.09.27
申请号 RU20030109359 申请日期 2003.04.03
申请人 发明人 KRAVCHUK S.V.;PUCHKOV A.M.;SYROV A.S.
分类号 G05D1/08 主分类号 G05D1/08
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