An air data system for an aircraft (10) includes a multi-function probe (MFP) (12A, 12B, 12C) and an inertial reference unit (IRU) (14). The MFP (12A, 12B, 12C) is positioned to sense a pressure of airflow about an exterior of the aircraft (10). A first electronics channel (51) of the MFP (12A, 12B, 12C) is electrically coupled to the IRU (14) to generate air data parameter outputs based on the pressure sensed by the MFP (12A, 12B, 12C) and inertial data sensed by the IRU (14).
DUAL CHANNEL AIR DATA SYSTEM WITH INERTIALLY COMPENSATED BACKUP CHANNEL
ZWEIKANALIGES LUFTDATENSYSTEM MIT TRÄGE KOMPENSIERTEM BACKUP-KANAL
SYSTÈME DE DONNÉES D'AIR À DOUBLE CANAL COMPRENANT UN CANAL DE SAUVEGARDE À COMPENSATION INERTIELLE
2019-12-18
Patent
Electronic Resource
English
DUAL CHANNEL AIR DATA SYSTEM WITH INERTIALLY COMPENSATED BACKUP CHANNEL
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