Fault Tolerant Flight Control A Benchmark Challenge /

• Συγγραφή απο Οργανισμό/Αρχή: SpringerLink (Online service)
• Άλλοι συγγραφείς: Edwards, Christopher (Επιμελητής έκδοσης), Lombaerts, Thomas (Επιμελητής έκδοσης), Smaili, Hafid (Επιμελητής έκδοσης)
• Μορφή: Ηλεκτρονική πηγή Ηλ. βιβλίο
• Γλώσσα: English
• Έκδοση: Berlin, Heidelberg : Springer Berlin Heidelberg, 2010.
• Σειρά: Lecture Notes in Control and Information Sciences, 399
• Θέματα: Engineering.; System theory.; Automotive engineering.; Aerospace engineering.; Astronautics.; Control engineering.; Robotics.; Mechatronics.; Electronics.; Microelectronics.; Aerospace Technology and Astronautics.; Electronics and Microelectronics, Instrumentation.; Control, Robotics, Mechatronics.; Systems Theory, Control.; Automotive Engineering.

The European Flight Mechanics Action Group FM-AG(16) on Fault Tolerant Control, established in 2004 and concluded in 2008, represented a collaboration involving thirteen European partners from industry, universities and research establishments under the auspices of the Group for Aeronautical Researc...

Πίνακας περιεχομένων:

• 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.