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公开(公告)号：US20240321125A1
公开(公告)日：2024-09-26
申请号：US18608913
申请日：2024-03-18
Applicant: DASSAULT AVIATION
Inventor： Stéphane PICAUT , Yann COUREAUD
CPC classification number: G08G5/025 , G08G5/0021 , G08G5/0047
Abstract: A method for assisting an aircraft in landing on a runway and an associated system includes determining a target exit point from the runway and a target taxi speed at which the aircraft has to take the target exit; calculating a target ground distance representative of a ground deceleration phase; and calculating the position of a target touchdown point on the basis of the target ground distance. The target ground distance is calculated as a function of a target deceleration profile for the aircraft to reach the target exit point at the target taxi speed.
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