Novel robust fault diagnosis method for flight control systems

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摘要 Anovelrobustfaultdiagnosisscheme,whichpossessesfaultestimatecapabilityaswellasfaultdiagnosisproperty,isproposed.Theschemeisdevelopedbasedonasuitablecombinationoftheadaptivemultiplemodel(AMM)andunknowninputobserver(UIO).ThemainideaoftheproposedschemestemsfromthefactthattheactuatorLock-in-Placefaultisunknown(whenandwheretheactuatorgetslockedareunknown),andmultiplemodelsareusedtodescribedifferentfaultscenarios,thenabankofunknowninputobserversaredesignedtoimplementthedisturbancede-coupling.AccordingtoLyapunovtheory,proofoftherobustnessofthenewlydevelopedschemeinthepresenceoffaultsanddisturbancesisderived.Numericalsimulationresultsonanaircraftexampleshowsatisfactoryperformanceoftheproposedalgorithm.
机构地区 不详
出版日期 2008年05月15日(中国期刊网平台首次上网日期,不代表论文的发表时间)
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