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- W1569114388 abstract "The aim of this paper is to identify an LFT model of a rigid aircraft. The highly structured aerodynamic model is first put under a standard LFT form, in which the uncertain parameters are gathered inside a full real block A. Time domain measurements are then translated into frequency domain ones, using a classical FFT technique. Under a rank condition which is satisfied in our aircraft application, inputs and outputs of the model perturbation A can be deduced from the physical aircraft inputs and outputs, so that A can be identified using either a Robust Least Squares method, or an output error set-membership identification technique." @default.
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- W1569114388 date "2001-09-01" @default.
- W1569114388 modified "2023-09-23" @default.
- W1569114388 title "Frequency domain identification of an aircraft LFT model" @default.
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- W1569114388 doi "https://doi.org/10.23919/ecc.2001.7075984" @default.
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