Invention Grant
US09142135B2 Method and device for automatically determining an optimized approach and/or descent profile 有权
用于自动确定优化方法和/或下降轮廓的方法和装置

Method and device for automatically determining an optimized approach and/or descent profile
Abstract:
A method and device for automatically determining an optimized approach and/or descent profile for an aircraft are provided. The device comprises means for optimizing an approach and/or descent profile of an aircraft avoiding long and steep geometric segments, the device to this end inserting an idle segment, if it satisfies the restrictions, in the profile relating to the descent phase and/or to the approach phase, wherein said idle segment can be followed by a geometric segment.
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