Estimation of a criterion of load to which a structural component of an aircraft is subjected, and assistance for the detection of a so-called“hard”landing by virtue of such a criterion

摘要

A method for estimating a loading criterion relating to the load experienced by a structural component of an aircraft, and assistance with detecting a so-called“hard”landing. The method includes measuring parameters of the aircraft and calculating at least one loading criterion for the loading of the structural component using at least one neural network receiving the parameters as input. Assistance with detecting a hard landing then includes determining of a time of impact of the aircraft on a landing strip from the measured parameters, then estimating a plurality of the parameters at the determined time of impact so as to calculate the at least one loading criterion relating to the loading of the structural component.