Development and Evaluation of an Integral Sliding Mode Fault Tolerant Control Scheme on the RECONFIGURE Benchmark
- Submitting institution
-
University of Exeter
- Unit of assessment
- 12 - Engineering
- Output identifier
- 2066
- Type
- D - Journal article
- DOI
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10.1002/rnc.3951
- Title of journal
- International Journal of Robust and Nonlinear Control
- Article number
- -
- First page
- 5314
- Volume
- 29
- Issue
- 16
- ISSN
- 1049-8923
- Open access status
- Compliant
- Month of publication
- October
- Year of publication
- 2017
- URL
-
-
- Supplementary information
-
-
- Request cross-referral to
- -
- Output has been delayed by COVID-19
- No
- COVID-19 affected output statement
- -
- Forensic science
- No
- Criminology
- No
- Interdisciplinary
- No
- Number of additional authors
-
2
- Research group(s)
-
D - Dynamics and Control
- Proposed double-weighted
- No
- Reserve for an output with double weighting
- No
- Additional information
- The technology developed here is part of EU-FP7 RECONFIGURE project (EUR3.7M) which addressed a key industrial challenge to design a resilient flight control that directly handles loss of sensor measurements. The technology was rigorously evaluated by AIRBUS and forms a key part in the final public workshop at AIRBUS Toulouse (P.Goupil*). This work led to participation in the VISION project co-funded by EU-H2020/NEDO-Japan (EUR1.8M). The work led to a world-first demonstration of an increase in TRL level by piloted flight tests conducted in Japan between 2017-2019 on JAXA's MuPAL-alpha experimental fly-by-wire aircraft (M.Sato**). * philippe.goupil@airbus.com. ** sato.masayuki@jaxa.jp
- Author contribution statement
- -
- Non-English
- No
- English abstract
- -
