G - Physics – 01 – C
Patent
G - Physics
01
C
G01C 23/00 (2006.01) B64D 43/00 (2006.01) G01C 25/00 (2006.01)
Patent
CA 2683254
The invention relates to a integrated standby instrument and a calibration method for the integrated standby instrument. Such an instrument allows flight information to be determined and displayed in a stand--alone manner. It is employed in the case of failure of the primary instruments of the aircraft. The object of the invention consists in determining and in displaying, also in a stand-alone manner, a heading followed by the aircraft. For this purpose, a computer (28) in the instrument (10) allows a heading of the aircraft to be determined using a magnetic field sensor and allows the magnetic field sensor to be calibrated. The screen of the instrument (10) allows the heading and a guide for the calibration of the magnetic field sensor to be displayed.
Colliau Florent
Hemelsdael Charles
Marks & Clerk
Thales
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