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
- Patent Title: Method for aiding navigation for an aircraft during descent and during approach at reduced thrust
- Patent Title (中): 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
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Application No.: US14522469Application Date: 2014-10-23
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Publication No.: US09188978B2Publication Date: 2015-11-17
- Inventor: Jerome Sacle , Johan Boyer , Francois Coulmeau
- Applicant: THALES
- Applicant Address: FR Courbevoie
- Assignee: THALES
- Current Assignee: THALES
- Current Assignee Address: FR Courbevoie
- Agency: Baker & Hostetler LLP
- Priority: FR1302471 20131025
- Main IPC: G05D1/00
- IPC: G05D1/00 ; G05D1/04 ; G08G5/00 ; G01C21/20 ; G05D1/06 ; G06Q10/04 ; G08G5/02

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.
Public/Granted literature
- US20150120100A1 METHOD FOR AIDING NAVIGATION FOR AN AIRCRAFT DURING DESCENT AND DURING APPROACH AT REDUCED THRUST Public/Granted day:2015-04-30
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