Method for determining an aircraft trajectory exhibiting noise reduction on takeoff with a floor slope, method, determination system and associated aircraft

Abstract

Method for determining an aircraft trajectory exhibiting noise abatement on takeoff with a minimum gradient, method, determination system and associated aircraft. The determination method is implemented using a determination system and comprises the following steps: - determination of characteristics of an initial trajectory segment (22) flown at maximum thrust to a predefined minimum altitude (23); - determination of characteristics of at least one trajectory segment exhibiting noise abatement (24, 26) with reduced thrust relative to maximum thrust to reach a target speed; - definition of at least one minimum gradient to be maintained by the aircraft corresponding to the trajectory segment(s) exhibiting noise abatement (24, 26). Figure for the abstract: Figure 3

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