Fault Tolerant Flight Control
[BOOK DESCRIPTION]
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.
[TABLE OF CONTENTS]
Surviving the Improbable: Towards Resilient Aircraft Control.
- Fault Tolerant Flight Control
- A Survey.
- Fault Detection and Diagnosis for Aeronautic and Aerospace Missions.
- Real-Time Identification of Aircraft Physical Models for Fault Tolerant Flight Control.
- Industrial Practices in Fault Tolerant Control.- RECOVER: The Benchmark Challenge.
- RECOVER: A Benchmark for Integrated Fault Tolerant Flight Control Evaluation.
- Assessment Criteria as Specifications for Reconfiguring Flight Control.
- Design Methods and Benchmark Analysis.- Fault Tolerant Control Using Sliding Modes with On-Line Control Allocation.
- An Adaptive Fault-Tolerant FCS for a Large Transport Aircraft.- Subspace Predictive Control Applied to Fault-Tolerant Control.- Fault-Tolerant Control through a Synthesis of Model-Predictive Control and Nonlinear Inversion.
- A FTC Strategy for Safe Recovery against Trimmable Horizontal Stabilizer Failure with Guaranteed Nominal Performance.
- Flight Control Reconfiguration Based on Online Physical Model Identification and Nonlinear Dynamic Inversion.
- A Combined Fault Detection, Identification and Reconfiguration System Based around Optimal Control Allocation.
- Detection and Isolation of Actuator/Surface Faults for a Large Transport Aircraft.- Real-Time Flight Simulator Assessment.- Real-Time Assessment and Piloted Evaluation of Fault Tolerant Flight Control Designs in the SIMONA Research Flight Simulator.
- Piloted Evaluation Results of a Nonlinear Dynamic Inversion Based Controller Using Online Physical Model Identification.
- Model Reference Sliding Mode FTC with SIMONA Simulator Evaluation: EL AL Flight 1862 Bijlmermeer Incident Scenario.
- Conclusions.
- Industrial Review.
- Concluding Remarks.
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