Flying process and device of an aircraft optimizing the...

B - Operations – Transporting – 64 – C

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B64C 9/06 (2006.01) B64C 13/16 (2006.01) B64C 13/50 (2006.01) G05D 1/06 (2006.01) G05D 1/08 (2006.01)

Patent

CA 2647478

In conformance with the invention, based on the incident conditions and velocity, the steering of the ailerons is weakly negative (b0) or corresponds either to the maximum sharpness of the aircraft (b1), or the optimal lift of the latter (b2).

Conformément à l'invention, selon des conditions de vitesse et d'incidence, le braquage des ailerons est faiblement négatif (bO) ou correspond soit à la finesse maximale de l'aéronef (b1), soit à la portance optimale de ce dernier (b2).

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