发明名称 Control device with servocontrol loop, particularly an electro-hydraulic flight control actuator
摘要 A control device includes a main servocontrol loop having a servocontrolled system, and a compensation device on the input side of the control device. The control device includes an internal loop that receives a first signal derived from the main servocontrol loop as input, and generates, as a function firstly of the first signal and secondly of a second signal characteristic of a parameter of the servocontrolled system, an error signal characteristic of the difference between said second signal and a theoretical signal determined using a model. The error signal being injected into the main servocontrol loop to correct the control of the servocontrolled system. The internal loop and/or the main loop include a variable gain amplifier, and the control device controls the gain of the variable gain amplifier.
申请公布号 US7139643(B2) 申请公布日期 2006.11.21
申请号 US20030346827 申请日期 2003.01.17
申请人 TRW SYSTEMES AERONAUTIQUES CIVILS 发明人 SILVESTRO GENEVIEVE
分类号 G05D3/12;G05B13/04;G05B19/19;G05D1/08;G06F19/00 主分类号 G05D3/12
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