US 12709380 B2 / Aug 18, 2026

Electrical servo system for a flight control surface, method of detecting sensor failure, and method for determining correct function of a movement related flight control surface sensor

Electrical servo system for a flight control surface comprising: a flight control surface moveable with respect to a mounting portion; an electric actuator configured to actuate the flight control surface; at least one movement-related flight control surface sensor, which is configured to acquire a quantity related to a movement of the flight control surface; at least one movement-related actuator sensor, which is configured to acquire a quantity related to a movement of the actuator. In order to enhance control accuracy, a controller is provided, which is configured to control according to a cascaded closed loop control, wherein the at least one movement-related flight control surface sensor is used in an outer closed loop control for movement control of the flight control surface, and the at least one movement-related actuator sensor is used in an inner closed loop control for movement control of the actuator.

Publication details

Recorded assignee
ARCHER AVIATION INC.
Publication number
US 12709380 B2
Publication type
Utility patent grant
Publication date
Aug 18, 2026
Filing date
Mar 12, 2024
CPC classes
B64C13/50, B64D45/00, B64D45/0005, B64F5/60, B64C11/001, B64C29/0033, B64C39/12, B64D27/34, B64D2045/0085
Inventors
Wu; Eric, Wurdak; Philipp

Party names reflect the published document. Current ownership and legal status can change.

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