Optimum strategies for selecting descent flight-path angles
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United States of America Patent
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Aug 23, 2016
Grant Date -
N/A
app pub date -
Aug 11, 2014
filing date -
Aug 12, 2013
priority date (Note) -
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Abstract
An information processing system and method for adaptively selecting an aircraft descent flight path for an aircraft, are provided. The system receives flight adaptation parameters, including aircraft flight descent time period, aircraft flight descent airspace region, and aircraft flight descent flyability constraints. The system queries a plurality of flight data sources and retrieves flight information including any of winds and temperatures aloft data, airspace/navigation constraints, airspace traffic demand, and airspace arrival delay model. The system calculates a set of candidate descent profiles, each defined by at least one of a flight path angle and a descent rate, and each including an aggregated total fuel consumption value for the aircraft following a calculated trajectory, and a flyability constraints metric for the calculated trajectory. The system selects a best candidate descent profile having the least fuel consumption value while the flyability constraints metric remains within aircraft flight descent flyability constraints.

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Patent Owner(s)
Patent Owner | Address | |
---|---|---|
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION (NASA) | WASHINGTON DC |
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Inventor(s)
Inventor Name | Address | # of filed Patents | Total Citations |
---|---|---|---|
Green, Steven M | - | 5 | 151 |
Wu, Minghong G | Sunnyvale, US | 1 | 19 |
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