Invention Grant
- Patent Title: Navigation assistance method for monitoring navigation performance in linear or angular mode
- Patent Title (中): 用于监视线性或角度模式导航性能的导航辅助方法
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Application No.: US13797485Application Date: 2013-03-12
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Publication No.: US08948939B2Publication Date: 2015-02-03
- Inventor: Guilhem Putz , Christophe Caillaud , Francois Coulmeau
- Applicant: Thales
- Applicant Address: FR Neuilly sur Seine
- Assignee: Thales
- Current Assignee: Thales
- Current Assignee Address: FR Neuilly sur Seine
- Agency: Baker Hostetler LLP
- Priority: FR1200755 20120313
- Main IPC: G06F19/00
- IPC: G06F19/00 ; G08G5/00 ; G01C23/00 ; G05D1/06 ; G05D1/10 ; G08G5/02 ; G05D1/02

Abstract:
A method for assisting in the navigation of an aircraft comprises steps of calculating and displaying a linear deviation on a first linear section and an angular deviation on a second angular section. The method comprises a calculation step for converting an angular deviation into an equivalent linear deviation, and, conversely, converting a linear deviation into an equivalent angular deviation. The method comprises a step of graphic representation, called unified monitoring, intended for the crew, of a deviation of the aircraft, on a lateral deviation axis and a vertical deviation axis; each of the deviations, lateral and vertical, being able to be represented on a linear scale, an angular scale or a mixed scale.
Public/Granted literature
- US20130245861A1 Navigation Assistance Method for Monitoring Navigation Performance in Linear or Angular Mode Public/Granted day:2013-09-19
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