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SPACE PATENTS BY
Aerospace Assignees
Aerospace Inventors
Time Lines

Control device with servocontrol loop, particularly an electro-hydraulic flight control actuator

Invented by: Genevieve Silvestro
Eragny, FR

Originally Assigned to: TRW Systemes Aeronautiques Civils
Saint-Quen l'Aumone, FR
[Now assigned to . . .]

Issued:2006-11-21
Filed:2003-01-17
Application No:10346827
Examined by:Nguyen; Tan Q.

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.

[pdf] U.S. Pat. No. 7,139,643

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This information is part of a study by Oasis Global, Inc. of all space inventions filed at the United States Patent and Trademark Office, and is provided for informational purposes only. It is not an endorsement of any particular assignee, inventor or invention. Although Peter A. Koziol represents inventors and assignees of space inventions he does not represent all of the inventors and assignees listed. The prosecuting attorney agent or firm for each patent is identified by the United States Patent and Trademark Office in the patent specfication, which can be viewed by clicking on the patent image or downloading the patent document. For more information regarding Mr. Koziol's background and experience, or to learn more about space inventions, please contact Mr. Koziol.

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