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Robust detection, isolation and accommodation for sensor failuresThe objective is to extend the recent advances in robust control system design of multivariable systems to sensor failure detection, isolation, and accommodation (DIA), and estimator design. This effort provides analysis tools to quantify the trade-off between performance robustness and DIA sensitivity, which are to be used to achieve higher levels of performance robustness for given levels of DIA sensitivity. An innovations-based DIA scheme is used. Estimators, which depend upon a model of the process and process inputs and outputs, are used to generate these innovations. Thresholds used to determine failure detection are computed based on bounds on modeling errors, noise properties, and the class of failures. The applicability of the newly developed tools are demonstrated on a multivariable aircraft turbojet engine example. A new concept call the threshold selector was developed. It represents a significant and innovative tool for the analysis and synthesis of DiA algorithms. The estimators were made robust by introduction of an internal model and by frequency shaping. The internal mode provides asymptotically unbiased filter estimates.The incorporation of frequency shaping of the Linear Quadratic Gaussian cost functional modifies the estimator design to make it suitable for sensor failure DIA. The results are compared with previous studies which used thresholds that were selcted empirically. Comparison of these two techniques on a nonlinear dynamic engine simulation shows improved performance of the new method compared to previous techniques
Document ID
19860021260
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Emami-Naeini, A.
(Systems Control Technology, Inc. Palo Alto, CA, United States)
Akhter, M. M.
(Systems Control Technology, Inc. Palo Alto, CA, United States)
Rock, S. M.
(Systems Control Technology, Inc. Palo Alto, CA, United States)
Date Acquired
September 5, 2013
Publication Date
July 1, 1986
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
SCT-85-5449
NAS 1.26:174825
NASA-CR-174825
Report Number: SCT-85-5449
Report Number: NAS 1.26:174825
Report Number: NASA-CR-174825
Accession Number
86N30732
Funding Number(s)
CONTRACT_GRANT: NAS3-24079
PROJECT: RTOP 505-34-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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