Aeronautical display system and method
AssigneeMilton Academy
InventorsDaming Cui, Noah Shane Fuller, Sarah Ting-Ting Hsu, Patrick Jiacheng Huang, Max Hui, Bradley Moriarty
Life of this patent
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Abstract
A computer-implemented method, computer program product and computing system for receiving a current operating value concerning an operating condition of an aircraft; rendering the current operating value within a magnified operating window of a glass cockpit of the aircraft; and locating the magnified operating window along a fixed range of operating values for the aircraft based, at least in part, upon the current operating value.
Claims18
A computer-implemented method, executed on a computing device, comprising:
- receiving a current operating value concerning an operating condition of an aircraft;
- rendering the current operating value within a magnified operating window of a glass cockpit of the aircraft;
- and
- locating the magnified operating window along a fixed range of operating values for the aircraft based, at least in part, upon the current operating value,
- wherein the current operating value is an airspeed of the aircraft and the fixed range of operating values is a range of possible airspeeds for the aircraft, or
- wherein the current operating value is an altitude of the aircraft and the fixed range of operating values is a range of possible altitudes for the aircraft.
A non-transitory computer program product residing on a computer readable medium having a plurality of instructions stored thereon which, when executed by a processor, cause the processor to perform operations comprising:
- receiving a current operating value concerning an operating condition of an aircraft;
- rendering the current operating value within a magnified operating window of a glass cockpit of the aircraft;
- and
- locating the magnified operating window along a fixed range of operating values for the aircraft based, at least in part, upon the current operating value,
- wherein the current operating value is an airspeed of the aircraft and the fixed range of operating values is a range of possible airspeeds for the aircraft, or
- wherein the current operating value is an altitude of the aircraft and the fixed range of operating values is a range of possible altitudes for the aircraft.
A computing system including a processor and memory configured to perform operations comprising:
- receiving a current operating value concerning an operating condition of an aircraft;
- rendering the current operating value within a magnified operating window of a glass cockpit of the aircraft;
- and
- locating the magnified operating window along a fixed range of operating values for the aircraft based, at least in part, upon the current operating value,
- wherein the current operating value is an airspeed of the aircraft and the fixed range of operating values is a range of possible airspeeds for the aircraft, or
- wherein the current operating value is an altitude of the aircraft and the fixed range of operating values is a range of possible altitudes for the aircraft.
Dependencies are inferred from the claim text.