Method and device for flying an aircraft according to at...

G - Physics – 05 – D

Patent

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G05D 1/08 (2006.01)

Patent

CA 2616185

The inventive device (1) comprises means (2) for determining a control value corresponding to an instruction value representing the actuation of a control member (3) by a pilot, means (5) for controlling an effective control value corresponding to said instruction value which is actually applied to the aircraft, means (6) for automatically controlling the aircraft, means (11) for computing an auxiliary control value, which is closer to the effective controlled value and means (16) for monitoring the control value and for detecting a pilot induced oscillation, wherein the automatic control is carried out with the aid of the controlled effective value and the auxiliary control value in the case of the detection of the pilot induced oscillation.

Procédé et dispositif de pilotage d'un aéronef selon au moins un axe de pilotage. Le dispositif (1 ) comporte des moyens (2) pour déterminer une valeur de commande correspondant à la valeur d'un ordre représentatif de l'actionnement d'un organe de commande (3) par un pilote, des moyens (5) déterminant une valeur effective commandée correspondant à la valeur dudit ordre, effectivement appliquée à l'aéronef, des moyens (6) réalisant, à l'aide de la valeur de commande et de la valeur effective commandée, un asservissement de l'aéronef, des moyens (1 1 ) calculant une valeur de commande auxiliaire qui est plus proche de la valeur effective commandée que la valeur de commande, et des moyens (1 1 ) surveillant la valeur de commande et permettant de détecter un pompage piloté, l'asservissement étant réalisé à l'aide de la valeur effective commandée et de la valeur de commande auxiliaire en cas de détection d'un pompage piloté.

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