Publisher URL: https://patents.google.com/patent/US9321543B2
https://depatisnet.dpma.de/DepatisNet/depatisnet?action=bibdat&docid=US000009321543B2
Title: Method and device for condition monitoring
Language: English
Authors: Randerath, Bernhard 
Gerdes, Mike 
Scholz, Dieter  
Other : Airbus Operations GmbH 
Keywords: aircraft; spacecraft; test; inspection; condition monitoring; decision tree; classification function
Issue Date: 26-Apr-2016
Is supplemented by: http://hdl.handle.net/20.500.12738/1093
Abstract: 
A computer-implemented method, a computer program product and a device for the condition monitoring of a component or system, such as for an aircraft or spacecraft. The method includes: providing an optimized decision tree, the nodes of which contain attributes of an input vector, the leaves of which each contain a classification function and the connections of which between the nodes are weighted; providing an input vector derived from a data signal; implementing a condition monitoring in which the condition of the component or system is determined using the weighted decision tree and on the basis of the input vector. In addition to an item of information concerning which of the classification functions of the decision tree best corresponds to the input vector, an additional item of information concerning the probability with which the other classes of the decision tree correspond to the examined input vector is calculated and output.
URI: https://hdl.handle.net/20.500.12738/16269
Review status: This version was reviewed (alternative review procedure)
Institute: Forschungsgruppe Flugzeugentwurf und -systeme (AERO) 
Department Fahrzeugtechnik und Flugzeugbau 
Fakultät Technik und Informatik 
Type: Patent
Additional note: AIRBUS OPERATIONS, 2016. Method and Device for Condition Monitoring. Inventors: RANDERATH, Bernhard, GERDES, Mike, SCHOLZ, Dieter. Application: 2012-05-30, US20140163812A1. US Patent, US9321543B2, 2016-04-26. Available from: https://patents.google.com/patent/US9321543B2.
Patent ID: US9321543B2
US20140156570A1
DE102011076780B4
CN103597417B
WO2012163985A1
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