Systems and methods for airport selection and display of range remaining during engine out conditions
AssigneeHoneywell International Inc.
InventorsMichael Mast, Yuta Morioka, Martin Jezek, Jeffrey Glenn
Life of this patent
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AssigneeHoneywell International Inc.
InventorsMichael Mast, Yuta Morioka, Martin Jezek, Jeffrey Glenn
Estimating the term…
Flight guidance systems and methods that provide an airport selection in response to an EO condition in a single engine plane. The airport selection takes into consideration factors such as optimal approach type, runway length, weather, terrain, remaining battery time, and the like. Additionally, various also generate and display a visual indication of a remaining glide range when the EO condition is happening; the remaining glide range determination is based, at least in part, on terrain.
A flight guidance system for airport selection during engine out (EO) conditions in an aircraft, the system comprising:
A method for flight guidance for airport selection during engine out (EO) conditions in an aircraft, the method comprising:
Dependencies are inferred from the claim text.