General Electric Company

Ge Aviation Systems Limited

Jennifer Ruth Cooper

So Young Kim

Michael Eric Figard

Norman Leonard Ovens

Alexander Kaber Carroll

Sundar Murugappan

Sharon Ann Green

Mark Lawrence Darnell

Mark Issac Snyder

George R Henderson

Aaron Todd Williams

Bernardo Pires

Courtney L Albers

Jeffrey Robert Winters

Clement Chunman Chi

Janine Xin Yue Zhu

Kristin Anderson-Barrett

Christopher Scott Sensing

Masaki Merritt Akiyama

Samuel Levulis

A dynamic human machine interface system includes a mission commander application (MCA) unit including a control processor, the MCA active on one vehicle of a plurality of mission member vehicles, the MCA unit in communication with a data store, the control processor accessing executable instructions that cause the control processor to direct operations of components of the MCA unit, an alternate scenario evaluation unit accessing at least one of mission parameter records and flight member data records in the data store to recalculate mission parameters, a dynamic video interface unit to render the recalculated mission parameters on a mission control dashboard (MCD), the MCD presented to the mission commander on a display unit of the one vehicle, the MCD including a plurality of display pane areas selectable by a user interaction with an interactive interface, and each display area configurable by the user interaction to change content of the display pane.

Decision support system for air missioncommander dynamic mission re-planning

Display screen with transitional graphical user interface

A method of monitoring a cockpit of an aircraft includes receiving, by one or more controllers, an image depicting an operator manipulated input device located within the cockpit. The method can include determining, by the one or more controllers, an observed state of the operator manipulated input device. In particular, the observed state can be based on the image. The method can include determining, by the one or more controllers, a sensed state of the operator manipulated input device. In particular, the sensed state can be based on data from a sensor. The method can include determining, by the one or more controllers, a mismatch between the observed and sensed states of the operator manipulated input device.

System and method for monitoring a cockpit of an aircraft

Systems and methods for controlling an aerial vehicle are provided. The method includes receiving a first signal from a first input device, wherein the first signal is related to a mode of a flight director. The method includes outputting a parameter on an output device, wherein the parameter is related to the mode. The method includes receiving a second signal from a second input device, wherein the second signal causes the parameter to change to a new parameter. The method includes outputting, by the one or more processors, the new parameter on the output device. The method includes receiving, by the one or more processors, a third signal from a third input device, wherein the aerial vehicle is controlled by the flight director based on the third signal, and wherein the second input device is mechanically coupled to the first input device and the third input device.

Integrated flight management system and flight director

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Walnut Creek, CA, United States of America

Jennifer Ruth Cooper