Flight evaluation of a sliding mode online control allocation scheme for fault tolerant control
- Submitting institution
-
University of Exeter
- Unit of assessment
- 12 - Engineering
- Output identifier
- 5150
- Type
- D - Journal article
- DOI
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10.1016/j.automatica.2020.108829
- Title of journal
- Automatica
- Article number
- ARTN 108829
- First page
- -
- Volume
- 114
- Issue
- -
- ISSN
- 0005-1098
- Open access status
- Compliant
- Month of publication
- April
- Year of publication
- 2020
- 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
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3
- Research group(s)
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D - Dynamics and Control
- Proposed double-weighted
- No
- Reserve for an output with double weighting
- No
- Additional information
- This is a culmination of 10 years continued development in the Technology Readiness Levels (TRL) of a fault tolerate flight controller developed at Exeter. This is a key output from a series of European grants worth £10m (ADDSAFE, RECONFIGURE and VISION) involving AIRBUS Toulouse (philippe.goupil@airbus.com) and Dassault. The paper describes piloted flight tests of the scheme on a Japan Aerospace Exploration Agency (Masayuki SATO sato.masayuki@jaxa.jp) test vehicle. This is a world first and a rare case when a design from academia reaches this TRL (>6). The results of this work were presented in an invited plenary talk at SAFEPROCESS 2018.
- Author contribution statement
- -
- Non-English
- No
- English abstract
- -