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NASA NTRS · 19910046007

Real-time diagnostics of the reusable rocket engine using on-line system identification

Abstract

A model-based failure diagnosis system has been proposed for real-time diagnosis of SSME failures. Actuation, sensor, and system degradation failure modes are all considered by the proposed system. In the case of SSME actuation failures, it was shown that real-time identification can effectively be used for failure diagnosis purposes. It is a direct approach since it reduces the detection, isolation, and the estimation of the extent of the failures to the comparison of parameter values before and after the failure. As with any model-based failure detection system, the proposed approach requires a fault model that embodies the essential characteristics of the failure process. The proposed diagnosis approach has the added advantage that it can be used as part of an intelligent control system for failure accommodation purposes.

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BibTeXRIS

Guo, T.-H., Merrill, W., Duyar, A.. 1990-01-01. Real-time diagnostics of the reusable rocket engine using on-line system identification. https://ntrs.nasa.gov/citations/19910046007

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