Fault Tolerant Flight Control : A Benchmark Challenge
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...
Enregistré dans:
| Auteur principal: | |
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| Autres auteurs: | , |
| Format: | Livre numérique |
| Langue: | Anglais |
| Publié: |
Berlin, Heidelberg :
Springer Berlin Heidelberg : Springer e-books
[20..].
Cham : Springer Nature |
| Collection: | Lecture Notes in Control and Information Sciences
399 |
| Sujets: | |
| Accès en ligne: | Accès sur la plateforme de l'éditeur Accès sur la plateforme Istex Accès Université d'Orléans Accès INSA CVL |
| Note: |
Archives Springer e-books (Licence nationale) Archives Springer e-books (Licence nationale) |
| Autres localisations: | Voir dans le Sudoc |
| Edition sous un autre format: | • Fault tolerant flight control, a benchmark challenge, Christopher Edwards, Thomas Lombaerts and Hafid Smaili, editors, Berlin, Springer, 2010, 1 vol. (XXII-586 p.), Lecture notes in control and information sciences, 978-3-642-11689-6 |
Table des matières:
- 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