Centre National De La Recherche Scientifique

Airbus Operations (s.a.s.)

Universitë De Bordeaux

Institut Polytechnique De Bordeaux

Universite De Bordequx

Université De Bordeaux I

Jérôme Cieslak

Philippe Goupil

Rémy Dayre

Ali Zolghadri

Anca Gheorghe

Hervé Le Berre

David Henry

Denis Efimov

The detecting means () comprise measuring means () adapted to measure and provide at least one raw data corresponding to an aircraft parameter, computing means () adapted to estimate at least one derivative of said raw data, and detecting means () adapted to detect a failure with the aid of said derivative, said computing means () being adapted to estimate said derivative by differentiation.

Method and device for detecting a failure on an aircraft

A system for detecting jamming and/or uncontrolled movement of an aircraft control surface includes first means for estimating the value of at least one parameter of an equation simulating the feedback loop dynamic of the control surface, according to a recursive autoregressive method with exogenous variable of RARX type in a recursive least squares way, and second means for detecting jamming and/or uncontrolled movement of the control surface, according to the estimated parameter value by the application of a decision test in the parametric space.

Method and system for detecting jamming and/or uncontrolled movement of an aircraft control surface

A detection device determines whether an uncontrolled movement of a control surface of an aircraft is occurring. The device includes means for calculating the difference between a theoretical command and an actual command in order to form a residual value, and means for detecting an uncontrolled movement of the control surface, if a comparison value depending on this residual value is greater than a threshold value If the comparison value is greater than the threshold value during a confirmation time, then the uncontrolled movement of the control surface of the aircraft is confirmed.

Method and device for detecting an uncontrolled movement 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.

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

Growing community of inventors

Talence, France

Jérôme Cieslak