An estimation system includes a module for measuring a current angle of attack and current flight parameters of the aircraft, a module for estimating a current lift coefficient of the aircraft from the current flight parameters and from a mass of the aircraft, a module for estimating an angle of attack for a zero lift from the current angle of attack, from the current lift coefficient and from a slope of an affine part of at least one theoretical curve describing a lift coefficient of the aircraft as a function of an angle of attack, a module for estimating the current position of the flaps of the aircraft from the angle of attack for a zero lift and a module for sending the current position of the flaps to a user device.
PROCÉDÉ ET SYSTÈME D'ESTIMATION DE LA POSITION DE VOLETS D'UN AÉRONEF
METHOD AND SYSTEM FOR ESTIMATING THE POSITION OF THE FLAPS OF AN AIRCRAFT
VERFAHREN UND SYSTEM ZUR POSITIONSABSCHÄTZUNG DER KLAPPEN EINES FLUGZEUGS
2020-03-04
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
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