Fault diagnosis benchmark for a rocket engine demonstrator
| Autor: | A. Iannetti, G. Ordonneau, Julien Marzat, L. Vingert, Hélène Piet-Lahanier |
|---|---|
| Přispěvatelé: | Centre National d'Etudes Spatiales - Direction Des Lanceurs. (CNES), ONERA - The French Aerospace Lab [Palaiseau], ONERA-Université Paris Saclay (COmUE), ONERA - The French Aerospace Lab [Châtillon] |
| Rok vydání: | 2015 |
| Předmět: |
020301 aerospace & aeronautics
0209 industrial biotechnology Engineering Test bench business.industry Redline [SPI.FLUID]Engineering Sciences [physics]/Reactive fluid environment CUSUM BENCHMARK 02 engineering and technology Kalman filter Fault (power engineering) AEROSPACE APPLICATIONS MODEL-BASED FAULT DIAGNOSIS [INFO.INFO-PF]Computer Science [cs]/Performance [cs.PF] Identification (information) 020901 industrial engineering & automation 0203 mechanical engineering 13. Climate action Control and Systems Engineering Benchmark (surveying) Rocket engine business Simulation |
| Zdroj: | IFAC-Papers IFAC-PapersOnLine, Elsevier, 2015, 48 (21), p. 895-900. ⟨10.1016/j.ifacol.2015.09.640⟩ |
| ISSN: | 2405-8963 |
| DOI: | 10.1016/j.ifacol.2015.09.640 |
| Popis: | International audience; A diagnosis benchmark was developed for the MASCOTTE test bench of ONERA/CNES. It consists of a CARINS Simulator of the bench, model-based fault diagnosis algorithms and firing tests results. The objective of this work was to demonstrate alternatives to the classical redline monitoring strategy used on the bench. A simplified model of the cooling circuit of the test bench was built and used to apply a parameter identification detection method and a Kalman filter. The diagnosis flags are obtained through analysis of the residuals via CUSUM tests. This article shows the results obtained and proposes an example of methodology to identify and validate performances of new diagnostic strategies. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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