Method for reconstructing gusts and structural loads at...

Details Method for reconstructing gusts and structural loads at... Method for reconstructing gusts and structural loads at...

B - Operations, Transporting

64

F

B64F 5/00 (2006.01) G06F 17/10 (2006.01) G06F 17/50 (2006.01)

Patent

CA 2627631

A method for reconstructing gusts and/or structural loads at aircraft, in particular passenger aircraft, characterised by the process steps: a) generating an observer on the basis of a nonlinear model of the aircraft which describes the movement of the aircraft in all six degrees of freedom (DoF) and the elastic motion of the aircraft structure; b) continuously supplying all the data and measurements substantial for the description of the state of the aircraft to the observer; c) calculating the gust velocities and structural loads (manoeuvre and gust loads) by the observer from the supplied data and measurements.

L'invention porte sur un procédé de reconstitution des rafales et/ou données structurelles s'appliquant à un aéronef, et en particulier à un avion de ligne comportant les étapes suivantes: a) création d'un observateur sur la base d'un modèle non linéaire de l'aéronef qui décrit les mouvements de l'aéronef dans les six degrés de liberté, et les mouvements élastiques de sa structure; b) fourniture continue à l'observateur de toutes les données et mesures permettant de décrire l'état de l'aéronef; et (c) calcul de la vitesse des rafales, et des charges structurelles (dues à la manoeuvre et aux rafales) par l'observateur à partir des données et mesures fournies.

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