Honeywell International Inc.

Dean Wilkens

Darrell Horner

Ronald Vaughan

Arthur D Beutler

Jacob Kirk Maxfield

Christopher Haraway

Kenneth O'Rourke

Roberto Gudino

A high-integrity electromechanical actuator control system includes a system function controller, a plurality of actuator controllers, and at least one electromechanical actuator. Each actuator controller includes a first controller, a second controller, and a duty cycle computation circuit. The first controller receives digital actuator control commands supplied from two of the function control channels and supplies first digital duty cycle commands. The second controller receives digital actuator control commands supplied from two function control channels and supplies second digital duty cycle commands. The duty cycle computation circuit receives the first digital duty cycle commands and the second digital duty cycle commands, computes an average of the first and second duty cycle commands, and generates pulse width modulated (PWM) commutation control signals based on the computed average.

High-integrity actuator controller and control systems

Flight display systems and methods for displaying simplified primary flight information for an urban air mobility vehicle (UAMV). Embodiments provide a primary flight display with an enhanced human-machine interface to support the intuitive operation of the UAMV commensurate with an expected reduced training background of the operators.

Methods and systems for displaying simplified primary flight information for an urban air mobility vehicle (UAMV)

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Scottsdale, AZ, United States of America

Dean Wilkens