A method of assisting the piloting of an aircraft having at least one actuator acting on a control member. The aircraft has a main measurement system and a secondary measurement system respectively determining at least one predicted value and at least one measured value of a parameter that is used in at least one flight-control law. A filter unit is used to estimate an estimated value of at least one parameter with the help of the predicted and measured values, and for estimating at least one measurement accuracy margin. Each measurement accuracy margin is compared with a corresponding threshold, and the flight-control law that is to be applied is selected as a function of the comparison.
PROCEDE ET DISPOSITIF DE PILOTAGE D'UN AERONEF
2017-12-22
Patent
Elektronische Ressource
Französisch
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