An air data system for an aircraft includes a multi-function probe (MFP) and an inertial reference unit (IRU). The MFP is positioned to sense a pressure of airflow about an exterior of the aircraft. A first electronics channel of the MFP is electrically coupled to the IRU to generate air data parameter outputs based on the pressure sensed by the MFP and inertial data sensed by the IRU.
DUAL CHANNEL AIR DATA SYSTEM WITH INERTIALLY COMPENSATED BACKUP CHANNEL
SYSTEME DE DONNEES AERIENNES A DEUX CANAUX AVEC CANAL DE SECOURS COMPENSE PAR INERTIE
2019-12-15
Patent
Electronic Resource
English
IPC: | G01D MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE , Anzeigen oder Aufzeichnen in Verbindung mit Messen allgemein / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / G01K MEASURING TEMPERATURE , Messen der Temperatur |
DUAL CHANNEL AIR DATA SYSTEM WITH INERTIALLY COMPENSATED BACKUP CHANNEL
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