Air navigation device with inertial sensor units, radio...

Details Air navigation device with inertial sensor units, radio... Air navigation device with inertial sensor units, radio...

G - Physics

01

S

G01S 5/14 (2006.01) G01C 21/16 (2006.01)

Patent

CA 2653123

The present invention relates to an air navigation device with inertial sensor units and three-measuring-channel radio navigation receivers. It is characterised in that in two (10,12) of the three channels the inertial measuring units are ~low performance~ type MEMS with approximately 1°/h to 10°/h class gyro, the third channel comprising an inertial measuring unit (15) performing in compliance with standard ARINC 738.

La présente invention est relative à un dispositif de navigation aérienne à capteurs inertiels et récepteurs de radionavigation à trois voies de mesure, et elle est caractérisée en ce que dans deux (10, 12) des trois voies, les unités de mesure inertielle sont à MEMS de type <= basses performances >= à gyromètres de classe l°/h à 10°/h environ, la troisième voie comportant une unité de mesure inertielle (15) ayant des performances conformes à la norme ARINC 738.

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