TY - JOUR
T1 - The European ADDSAFE project
T2 - Industrial and academic efforts towards advanced fault diagnosis
AU - Goupil, Philippe
AU - Marcos, Andrés
PY - 2014/1/1
Y1 - 2014/1/1
N2 - In this article a high-fidelity aircraft benchmark, developed by Airbus for advanced flight control related studies, is presented in relation to its evolution towards advanced fault diagnosis within a European 7th Framework Program project entitled "Advanced Fault Diagnosis for Sustainable Flight Guidance and Control (ADDSAFE)". This European project was established to study and facilitate the transfer of model-based fault detection and diagnosis methods from Academia to Industry. The importance of the project arose on the one hand, due to the representativeness of the benchmark, and on the other hand, the industrial benchmarking and validation of the developed designs. The results presented in this article represent a quantitative measure of the success of the project since five of the developed designs were successfully validated in Airbus Verification and Validation (V&V) set-ups, and are currently undergoing further tests towards a possible real aircraft implementation.
AB - In this article a high-fidelity aircraft benchmark, developed by Airbus for advanced flight control related studies, is presented in relation to its evolution towards advanced fault diagnosis within a European 7th Framework Program project entitled "Advanced Fault Diagnosis for Sustainable Flight Guidance and Control (ADDSAFE)". This European project was established to study and facilitate the transfer of model-based fault detection and diagnosis methods from Academia to Industry. The importance of the project arose on the one hand, due to the representativeness of the benchmark, and on the other hand, the industrial benchmarking and validation of the developed designs. The results presented in this article represent a quantitative measure of the success of the project since five of the developed designs were successfully validated in Airbus Verification and Validation (V&V) set-ups, and are currently undergoing further tests towards a possible real aircraft implementation.
KW - European project
KW - Fault diagnosis
KW - Flight control
KW - Verification & validation
UR - http://www.scopus.com/inward/record.url?scp=84906780475&partnerID=8YFLogxK
U2 - 10.1016/j.conengprac.2014.03.011
DO - 10.1016/j.conengprac.2014.03.011
M3 - Article (Academic Journal)
AN - SCOPUS:84906780475
VL - 31
SP - 109
EP - 125
JO - Control Engineering Practice
JF - Control Engineering Practice
SN - 0967-0661
ER -