Ge Aviation Systems Limited

Paul Richard Hickman

George R Henderson

Luke Patrick Bolton

Systems and methods for correcting a vibration-induced error on a touch screen display device on an aircraft are provided. A method can include providing a user interface for display on a touch screen display device. The user interface can include one or more virtual elements associated with functions to be performed by a component of the aircraft. The method can include receiving data indicative of an actual user interaction with the touch screen display device. The method can include receiving data indicative of an intended user interaction. The method can include receiving data indicative of a sensed vibration. The method can include determining a corrected user interaction corresponding to a selected virtual element based on the data received. The method can also include sending one or more command signals to one or more components to perform a function associated with the selected virtual element.

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Cheltenham, United Kingdom

Paul Richard Hickman