Situational awareness, vehicle control, and/or contingency planning for aircraft actuator failure
AssigneeSkyryse, Inc.
InventorsMark Groden, Mitch Adler, Jonathan Reeves, Nur Harell, Christopher Ward
Life of this patent
Estimating the term…
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AssigneeSkyryse, Inc.
InventorsMark Groden, Mitch Adler, Jonathan Reeves, Nur Harell, Christopher Ward
Estimating the term…
An aircraft system of an aircraft may, while the aircraft is flying in a first flight mode, receive data from one or more sensors of the aircraft and, based on received data from one or more sensors, identify an actuation failure of an actuator of a flight control surface. The vehicle system may, subsequent to identifying the actuation failure of the actuator of the flight control surface, control the aircraft to fly in a modified flight mode. Controlling the aircraft to fly in the modified flight mode may include: determining a directional bias caused by the actuation failure, determining a modified flight plan based on the determined directional bias, and controlling the aircraft to fly based on the modified flight plan and the directional bias.
A non-transitory computer readable storage medium comprising stored instructions that, when executed by a set of one or more processors, cause the set of one or more processors to perform steps comprising:
A system comprising:
A system for an aircraft, the system comprising:
Dependencies are inferred from the claim text.