G - Physics – 01 – S
Patent
G - Physics
01
S
G01S 17/95 (2006.01)
Patent
CA 2568423
The invention relates to a system for measurement of projected turbulence downwind of an aircraft (14), arranged on board the same, comprising a lidar (10), emitting an optical beam (11) towards the front of the aircraft (14) and receiving a back-scattered optical beam (12), a direct detection device connected to control means, a first processing unit, using an internal correction algorithm and a second processing unit, using an external correction algorithm, which provide potential control signals for the actuators of at least one control surface (16) on the aircraft (14) .
L'invention concerne un système de mesure anticipée d'une turbulence en amont d'un aéronef (14) , disposé à bord de celui-ci, qui comprend un lidar (10) d'émission d'un faisceau optique (11) vers l'avant de l'aéronef (14) et de réception du faisceau optique rétrodiffusé (12) , un dispositif de détection directe associé à des moyens de contrôle, un premier organe de traitement utilisant un algorithme de corrections internes, et un second organe de traitement utilisant un algorithme de correction externes délivrant d'éventuels signaux de commandes aux actionneurs d'au moins une surface de contrôle (16) de l'aéronef (14) .
Aversa Nicky
Lacabanne Michel
Mirand Pierre
Airbus France
Airbus Operations Sas
Goudreau Gage Dubuc
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