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US Patent 10514707 Flight phase stability indicator system and method

Patent 10514707 was granted and assigned to Rockwell Collins on December, 2019 by the United States Patent and Trademark Office.

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Patent

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Current Assignee
Rockwell Collins
Rockwell Collins
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
10514707
Date of Patent
December 24, 2019
Patent Application Number
14315575
Date Filed
June 26, 2014
Patent Citations Received
‌
US Patent 12087170 Methods and systems for displaying simplified primary flight information for an urban air mobility vehicle (UAMV)
3
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US Patent 11790789 Gliding vertical margin guidance methods and systems
‌
US Patent 11927460 Control of diverse types of crew interface for flight control
4
Patent Primary Examiner
‌
Jacob S Scott
Patent abstract

A flight phase stability indicator system and method for generating and presenting stability indicator(s) are disclosed. A processor receives flight phase data representative of an identification of a current operational flight phase; receives navigation data comprised of aircraft position, a planned flight trajectory, and runway data if runway data is needed for the current operational flight phase; determines stability data representative of a stability of the current operational flight phase based upon at least the navigation data; generates presentation data responsive to the determination and representative of the flight phase stability indicator and/or presentation(s) of flight phase stability; and presents the indicator represented in the presentation data on or through a presentation unit comprised of a visual display, aural advisory unit, and/or tactile advisory unit.

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