US Patent 9849999 Avionics interface

Systems and methods are provided for an avionics interface of an aircraft. Sensors of the aircraft may convey information that can be used in the generation of one or more of the avionics interfaces. An avionics interface may include navigation information, engine instrument information, and communication information. Such information may be provided in visually distinct regions of the interface. An avionics interface may show an angle of attack of the aircraft in a visually incorporated manner with a navigation display. In some instances, the avionics interface may be variable to match pilot preference.