This is the english title

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B - Operations, Transporting

64

C

B64C 13/00 (2006.01) G01C 21/16 (2006.01)

Patent

CA 2418228

According to the invention, in this aircraft, the elements of the inertial reference system are separated according to whether they are intended for navigation (CI) or for flight (5, 6, 7). The accelerometers (5 and 6) intended for flight are located at a vibration antinode, and the gyrometers (7) intended for flight are located at a vibration node. The accelerometers (5 and 6) and gyrometers (7) are connected to the flight control computer (12) and their measurements are used as flight parameters.

Selon l'invention, dans cet aéronef, les éléments du système de réfé- rence inertielle sont séparés suivant qu'ils sont destinés à la navigation (CI) ou au pilotage (5, 6, 7). Les accéléromètres (5 et 6) destinés au pilotage sont disposés à un ventre de vibration, tandis que les gyromè- tres (7) destinés au pilotage sont placés à un noeud de vibration. Les ac- céléromètres (5 et 6) et les gyromètres (7) sont reliés au calculateur de commandes de vol (12) et leurs mesures servent comme paramètres de pilotage.

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