| 摘要 |
The general field of the invention relates to devices for controlling the two attitude reference units of the AHRS type for aircraft, each AHRS comprising at least a first set of magnetometer measurements and at least a second set of gyroscopic measurements, each AHRS having two modes of operation, the first mode, called slave mode supplying the flight system with the information coming from the first set, the second mode, called DG mode supplying the flight system with the information coming from the second set. The device according to the invention comprises a display and means for displaying within this display a control window for these two attitude reference units, said window comprising three regions, the first region dedicated to the first AHRS unit, the second region dedicated to the second AHRS unit, the third region dedicated to the simultaneous control of the two AHRS units.
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