2022
DOI: 10.1016/j.actaastro.2022.02.009
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Model-based supervised sensor placement optimization to detect propellant leak in a liquid rocket engine

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Cited by 10 publications
(2 citation statements)
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“…The second stage is a fault detection technology using signal processing and modeling analysis developed with the development of sensor technology; the third stage uses the core intelligent fault detection technology, such as data mining, deep learning, and information fusion. Scholars have different views on the classification of LRE fault diagnosis techniques [3,9,12,25,36,37]. In this paper, LRE fault detection approaches are divided into three types: signal processing-based approaches, model-driven approaches, and artificial intelligence-based approaches, which are shown in Figure 1.…”
Section: Summary Of State Of Fault Detection Technologymentioning
confidence: 99%
“…The second stage is a fault detection technology using signal processing and modeling analysis developed with the development of sensor technology; the third stage uses the core intelligent fault detection technology, such as data mining, deep learning, and information fusion. Scholars have different views on the classification of LRE fault diagnosis techniques [3,9,12,25,36,37]. In this paper, LRE fault detection approaches are divided into three types: signal processing-based approaches, model-driven approaches, and artificial intelligence-based approaches, which are shown in Figure 1.…”
Section: Summary Of State Of Fault Detection Technologymentioning
confidence: 99%
“…Specific to aerospace systems, there are also some related works. Omata et al [36] employed a greedy approach utilizing the detection performance score from multivariate supervised analysis for sensor placement optimization to identify propellant leaks in an LRE. Yang et al [37] reported a two-step strategy of non-probabilistic multi-objective optimization for load-dependent sensor placement with interval uncertainties to determine the final sensor configuration from a Pareto solution, and the accuracy of the proposed method was verified using an example involving space docking module in Space Power Satellites (SPSs).…”
Section: Introductionmentioning
confidence: 99%