SYSTEM AND METHOD FOR AIRCRAFT CONFIGURATION CHECKING

Abstract: the method can include: optionally determining an aircraft state; determining a transition event; verifying an aircraft configuration; determining an aircraft alert state; and performing an action. however, the method can additionally or alternatively include any other suitable elements. the method functions to facilitate configuration checking and/or validation of configuration changes. additionally or alternatively, the method can function to facilitate human-in-the-loop operation of a semi-autonomous aircraft (e.g., with an autonomous agent fulfilling the roles of one pilot of a multi-pilot aircraft). additionally or alternatively, the method can function to autonomously respond to inconsistencies or failures associated with aircraft configuration changes.

Inventor(s): Matthew George, Alexander Naiman, Angel Macias, Aubrey Kalashian, Kevin Elfenbein

CPC Classification: G05D1/2285 (SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES)

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