Invention Grant
US09188978B2 Method for aiding navigation for an aircraft during descent and during approach at reduced thrust 有权
在下降期间和在减小推力进近期间协助航空器导航的方法

Method for aiding navigation for an aircraft during descent and during approach at reduced thrust
Abstract:
A method for aiding navigation for an aircraft between a descent start point and a computation end point, comprises the computation steps of: collecting a flight plan consisting of a succession of waypoints and of the associated vertical constraints; determining a corridor consisting of a floor trajectory and of a ceiling trajectory defining the minimum and maximum altitudes permitted to the aircraft; splitting the corridor into several cells defined between two waypoints furthest apart and between which the ceiling trajectory is distinct from the floor trajectory; determining for at least one cell a vertical trajectory complying with the altitude constraints and comprising the longest possible IDLE segment; and a step consisting in determining and displaying maneuvering points of the aircraft making it possible to follow the target vertical trajectory.
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