Aircraft configuration management method and device
A device (1) for managing configurations of an aircraft between an initial point and a final point comprises a computation module (2) to determine at least one first evolution curve considering the aircraft to have assumed a first configuration and wherein the first evolution curve includes the firs...
Gespeichert in:
Hauptverfasser: | , , |
---|---|
Format: | Patent |
Sprache: | chi ; eng |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
Zusammenfassung: | A device (1) for managing configurations of an aircraft between an initial point and a final point comprises a computation module (2) to determine at least one first evolution curve considering the aircraft to have assumed a first configuration and wherein the first evolution curve includes the first point and a final evolution curve considering the aircraft to have assumed at least one final configuration and wherein the final evolution curve or curves includes the final point, a computation module (3) to compute at least one second point corresponding to the intersection of the first evolution curve or curves and the final evolution curve or curves, and a transmission module (4) configured to transmit a signal representing the coordinates of the second point or points to a user device (5).
种飞行器配置管理方法和设备。用于管理飞行器在起点与终点之间的配置的所述设备(1)包括:计算模块(2),所述计算模块用于确定至少个第演变曲线,考虑到所述飞行器已经采取了第配置并且所述第演变曲线包括所述第点,并且用于确定最终演变曲线,考虑到所述飞行器已经采取了至少个最终配置并且个或多个所述最终演变曲线包括所述终点;计算模块(3),所述计算模块用于计算至少个第二点,所述至少个第二点与个或多个所述第演变曲线和个或多个所述最终演变曲线的交叉点相对应 |
---|