Flight phase stability indicator system and method
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United States of America
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Jun 26, 2014
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Jun 26, 2014
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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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Family
- 15 United States
- 10 France
- 8 Japan
- 7 China
- 5 Korea
- 2 Other
Patent Owner(s)
- ROCKWELL COLLINS, INC.
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- [Patents Count]
Inventor(s)
Inventor Name | Address | # of filed Patents | Total Citations |
---|---|---|---|
Bell, Douglas A | Marion, US | 19 | 192 |
Carrico, Matthew J | Mt. Vernon, US | 22 | 328 |
Epperson, Kimm M | Springville, US | 2 | 7 |
Niraula, Madhu S | Cedar Rapids, US | 3 | 11 |
Sipper, Lori J | Robins, US | 3 | 11 |
Talbott, Curtis W | Cedar Rapids, US | 2 | 7 |
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