FLIGHT CONTROL SYSTEM WITH SYNTHETIC INTERTIAL LOCALIZER DEVIATION AND METHOD OF USE

FLIGHT CONTROL SYSTEM WITH SYNTHETIC INTERTIAL LOCALIZER DEVIATION AND METHOD OF USE

A flight control module for computing localizer deviation during landing of an aircraft is provided. The flight control module includes a communication interface and a processor. The communication interface is configured to receive inertial data for the aircraft. The processor is coupled to the comm...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: McLees, Robert E, Panyakeow, Prachya, Freeman, Robert Erik
Format: Patent
Sprache:eng
Schlagworte:
CONTROLLING
PHYSICS
REGULATING
SIGNALLING
SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
TRAFFIC CONTROL SYSTEMS
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Beschreibung
Zusammenfassung:A flight control module for computing localizer deviation during landing of an aircraft is provided. The flight control module includes a communication interface and a processor. The communication interface is configured to receive inertial data for the aircraft. The processor is coupled to the communication interface and is configured to compute an inertial localizer deviation based on the inertial data.