The European Flight Mechanics Action Group FM-AG(16) on Fault Tolerant C- trol, established in 2004 and concluded in 2008, represented a collaboration invo- ing thirteen European partners from industry, universities and research establi- ments under the auspices of the Group for Aeronautical Research and Technology 1 in Europe (GARTEUR) program .
In FM-AG(16) the following organizations p- ticipated: * Research Establishments - Centro Italiano Ricerche Aerospaziali (CIRA, Capua, Italy) - Deutsches Zentrum fur Luft-und Raumfahrt (DLR, Oberpfaffenhofen) - Defence Science and Technology Laboratory (DSTL, United Kingdom) - Netherlands National Aerospace Laboratory (NLR, Amsterdam) * Industry - QinetiQ (Bedford, United Kingdom) - Airbus (Toulouse, France) * Universities - Bordeaux University (LAPS, Bordeaux, France) - Delft University of Technology (DUT, Delft, the Netherlands) * Faculty of Aerospace Engineering (DUT-AE) * Delft Center of Systems and Control (DUT-DCSC) - Lille University (USTL, Lille, France) - University of Cambridge (UCAM, Cambridge, United Kingdom) 1 The Group for Aeronautical Research and Technology in EURope (GARTEUR) was formed in 1973 and has as member countries: France, Germany, the Netherlands, Spain, Sweden and the United Kingdom. According to its Memorandum of Understanding, the mission of GARTEUR is to mobilize, for the mutual bene?t of the GARTEUR member countries, their scienti?c and technical skills, human resources, and facilities in the ?eld of aeronautical research and technology.
Part I Surviving the Improbable: Towards Resilient Aircraft Control.- Introduction.- Fault Tolerant Flight Control - A Survey.- 3 Fault Detection and Diagnosis for Aeronautic and Aerospace.- Real-Time Identification of Aircraft Physical Models for Fault.- Industrial Practices in Fault Tolerant Control .- Part II RECOVER: The Benchmark Challenge.- RECOVER: A Benchmark for Integrated Fault Tolerant Flight.- Assessment Criteria as Specifications for Reconfiguring Flight.- Part III Design Methods and Benchmark Analysis .- Fault Tolerant Control Using Sliding Modes With On-line Control.- An Adaptive Fault-Tolerant FCS for a Large Transport Aircraft.- Subspace Predictive Control Applied to Fault-Tolerant Control .- A FTC Strategy for Safe Recovery Against Trimmable Horizontal.- Flight Control Reconfiguration based on Online Physical Model.- A Combined Fault Detection, Identification And Reconfiguration System Based Around Optimal Control Allocation.- Detection and Isolation of Actuator/Surface Faults for a Large.- Part IV Real-Time Flight Simulator Assessment.- Real-Time Assessment and Piloted Evaluation of Fault Tolerant.- Piloted Evaluation Results of a Nonlinear Dynamic Inversion based.- Model Reference Sliding Mode FTC with SIMONA Simulator.- Part V Conclusions.- Industrial review . - Concluding Remarks.
Series: Lecture Notes in Control and Information Sciences
Number Of Pages: 586
Published: 29th June 2010
Publisher: SPRINGER VERLAG GMBH
Country of Publication: DE
Dimensions (cm): 23.37 x 15.49
Weight (kg): 0.86