Process and device used to control the attitude of an aircraft

G - Physics – 05 – D

Patent

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G05D 1/08 (2006.01) B64C 13/00 (2006.01) B64C 13/20 (2006.01) B64D 1/02 (2006.01) B64D 1/12 (2006.01) G01C 21/20 (2006.01)

Patent

CA 2472316

- Le dispositif (1) comporte des spoilers (3) qui sont agencés sur les ailes (4) de l'avion, et dont les positions angulaires respectives peuvent être réglées par des actionneurs commandables (6), des moyens (8) pour déterminer une assiette de consigne de l'avion correspondant à une assiette que l'avion doit atteindre, des moyens (9) pour calculer des positions de consigne desdits spoilers (3), correspondant à des positions angulaires particulières desdits spoilers (3), permettant d'amener l'avion à ladite assiette de consigne, et des moyens (11) pour calculer des ordres de commande desdits actionneurs commandables (6), permettant d'amener lesdits spoilers (3) dans lesdites positions de consigne, lesdits ordres de commande étant appliqués auxdits actionneurs (6) desdits spoilers (3).

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