A first air data system for providing first aircraft air data parameter outputs is formed by a first electronics channel of a first multi-function probe (MFP) that is electrically coupled with a first electronics channel of a second MFP to receive static pressure data from the second MFP. A second air data system for providing second aircraft air data parameter outputs is formed by a second electronics channel of the second MFP that is electrically coupled with a second electronics channel of the first MFP to receive static pressure data from the first MFP. A third air data system for providing third aircraft air data parameter outputs is formed by a laser air data sensor that is configured to emit directional light into airflow about the aircraft exterior and to generate the third aircraft air data parameter outputs based on returns of the emitted directional light.
AIR DATA SYSTEM ARCHITECTURE INCLUDING PNEUMATIC AND LASER-BASED SENSOR MEASUREMENTS
ARCHITECTURE DE SYSTEME DE DONNEES COMPORTANT DES MESURES DE CAPTEUR FONDEES SUR UN DISPOSITIF PNEUMATIQUE ET UN LASER
2018-06-15
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
AIR DATA SYSTEM ARCHITECURE INCLUDING PNEUMATIC AND LASER-BASED SENSOR MEASUREMENTS
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