AIRBUS state of the art and practices on FDI and FTC in flight control system
- 17 April 2011
- journal article
- Published by Elsevier BV in Control Engineering Practice
- Vol. 19 (6), 524-539
- https://doi.org/10.1016/j.conengprac.2010.12.009
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- Oscillatory failure case detection in the A380 electrical flight control system by analytical redundancyControl Engineering Practice, 2010
- A novel non-linear observer-based approach to oscillatory failure detectionPublished by Institute of Electrical and Electronics Engineers (IEEE) ,2009
- Robust and Early Detection of Oscillatory Failure Case for New Generation Airbus AircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2008
- Airbus Fly-By-Wire: A Total Approach To DependabilityPublished by Springer Science and Business Media LLC ,2008
- Model-based fault-detection and diagnosis – status and applicationsAnnual Reviews in Control, 2005
- Triple-triple redundant 777 primary flight computerPublished by Institute of Electrical and Electronics Engineers (IEEE) ,2002
- Model-Based Fault Detection for an Actuator Driven by a Brushless DC MotorIFAC Proceedings Volumes, 1999
- Fly-by-wire for commercial aircraft: the Airbus experienceInternational Journal of Control, 1994
- Fault detection and diagnosis in aerospace systems using analytical redundancyComputing & Control Engineering Journal, 1991
- Fault diagnosis in dynamic systems using analytical and knowledge-based redundancy: A survey and some new resultsAutomatica, 1990