Method and Device for detecting the jamming of an aircraft control surface

The detection device includes, but is not limited to a device that is configured to determine a control error corresponding to the difference between a first control instruction and a control surface position, a second device that is configured to calculate the difference between this control error and a second control instruction in such a way as to form a comparison signal, and a third device that is configured to detect a jamming of the control surface if this comparison signal is greater than a threshold value.

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Source https://hal.science/hal-00825668
Author Goupil, Philippe, Dayre, Rémy, Gheorghe, Anca, Le Berre, Hervé, Zolghadri, Ali, Cieslak, Jérome, Henry, David
Maintainer CCSD
Last Updated May 11, 2026, 00:52 (UTC)
Created May 11, 2026, 00:52 (UTC)
Identifier Patent N°: United States Patent Application 20130116863
Language en
contributor Airbus France EYC - CC - Flight Control System ; Airbus France
creator Goupil, Philippe
date 2013-05-09T00:00:00
harvest_object_id 64ff0976-ea61-4642-a334-f3b11772845f
harvest_source_id 3374d638-d20b-4672-ba96-a23232d55657
harvest_source_title test moissonnage SELUNE
metadata_modified 2025-03-17T00:00:00
set_spec type:PATENT