Invention Grant
US07139643B2 Control device with servocontrol loop, particularly an electro-hydraulic flight control actuator
有权
具有伺服控制回路的控制装置,特别是电动液压飞行控制执行器
- Patent Title: Control device with servocontrol loop, particularly an electro-hydraulic flight control actuator
- Patent Title (中): 具有伺服控制回路的控制装置,特别是电动液压飞行控制执行器
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Application No.: US10346827Application Date: 2003-01-17
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Publication No.: US07139643B2Publication Date: 2006-11-21
- Inventor: Genevieve Silvestro
- Applicant: Genevieve Silvestro
- Applicant Address: FR Saint-Quen l'Aumone
- Assignee: TRW Systemes Aeronautiques Civils
- Current Assignee: TRW Systemes Aeronautiques Civils
- Current Assignee Address: FR Saint-Quen l'Aumone
- Agency: Blakely Sokoloff Taylor & Zafman
- Priority: FR0200679 20020121
- Main IPC: G05D3/12
- IPC: G05D3/12 ; G06F19/00

Abstract:
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.
Public/Granted literature
- US20060041339A1 Control device with servocontrol loop, particularly an electro-hydraulic flight control actuator Public/Granted day:2006-02-23
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