Method and device for aiding the approach of an aircraft during an approach phase for the purpose of landing
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United States of America Patent
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Jul 15, 2014
Grant Date -
Jun 14, 2012
app pub date -
Dec 2, 2011
filing date -
Dec 8, 2010
priority date (Note) -
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Abstract
The device includes elements of a processing unit which determine a limit trajectory representing a flight trajectory which is compatible with the aircraft performance during the approach and which shows the limits for the flight of the aircraft. For example, a vertical profile and a horizontal trajectory are determined, with the horizontal trajectory being non-linear so that the energy of the aircraft can be sufficiently dissipated before final approach along an approach axis, while also avoiding obstacles. Thus, a flight trajectory is determined even when the aircraft has deviated from a flight plan and approach axis.
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