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
15.12.2019
Patent
Elektronische Ressource
Englisch
IPC: | G01K MEASURING TEMPERATURE , Messen der Temperatur / G01D MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE , Anzeigen oder Aufzeichnen in Verbindung mit Messen allgemein / G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
DUAL CHANNEL AIR DATA SYSTEM WITH INERTIALLY COMPENSATED BACKUP CHANNEL
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