| 摘要 |
The invention relates to balancing a simulation platform (1) comprising a nonlinear aeronautical system (Mi, 20, 100). Balancing is based on: a servoing (200, 300) of an output value ({tilde over (Y)}, {tilde over (Y)}(−1)) of the system to a recorded value (Yk,cons(i), {tilde over (Y)}cons), comprising a first filter (300) producing an inversion of a simplified model (Fm, Gm) of the system for generating a said control (U) for the system based on a model correction information item (Δcorr) estimating a modeling error (Δm) of the simplified model (Fm, Gm) and an information item on difference (v) between the output value and the recorded value, and a modeling corrector looping comprising a second filter (400) using the said simplified model to calculate, based on the said control and the said output value, the model correction item to be supplied to the first filter.
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