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NASA NTRS ยท 19860003864

A preliminary evaluation of the generalized likelihood ratio for detecting and identifying control element failures in a transport aircraft

Abstract

The application of the Generalized Likelihood Ratio technique to the detection and identification of aircraft control element failures has been evaluated in a linear digital simulation of the longitudinal dynamics of a B-737 aircraft. Simulation results show that the technique has potential but that the effects of wind turbulence and Kalman filter model errors are problems which must be overcome.

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BibTeXRIS

Bundick, W. T.. 1985-09-01. A preliminary evaluation of the generalized likelihood ratio for detecting and identifying control element failures in a transport aircraft. https://ntrs.nasa.gov/citations/19860003864

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