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- W2007072527 abstract "This paper describes a reconfiguring flight control algorithm for damaged aircraft based upon a modular approach. This approach combines real time physical model identification with adaptive nonlinear dynamic inversion (NDI). The sensitivity of NDI to modeling errors is eliminated here by making use of a real time identified model of the aircraft. In failure situations, the damaged aircraft model is identified by the two step method and this updated model is supplied to the model-based adaptive NDI routine, which reconfigures for the fault in real time. Reconfiguration test results for damaged aircraft models indicate good fault handling capabilities of this fault tolerant control set-up, for component as well as structural faults." @default.
- W2007072527 created "2016-06-24" @default.
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- W2007072527 date "2011-06-01" @default.
- W2007072527 modified "2023-10-16" @default.
- W2007072527 title "Modular flight control reconfiguration design and simulation" @default.
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- W2007072527 doi "https://doi.org/10.1016/j.conengprac.2010.12.008" @default.
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