Invention Grant
US09395446B2 Onboard aircraft landing system, based on a GNSS system, with redundant and dissimilar architecture for high integrity level
有权
基于GNSS系统的机载飞机着陆系统,具有用于高完整性级别的冗余和不同的架构
- Patent Title: Onboard aircraft landing system, based on a GNSS system, with redundant and dissimilar architecture for high integrity level
- Patent Title (中): 基于GNSS系统的机载飞机着陆系统,具有用于高完整性级别的冗余和不同的架构
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Application No.: US13855430Application Date: 2013-04-02
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Publication No.: US09395446B2Publication Date: 2016-07-19
- Inventor: Stephane Rollet , Jean-Pierre Arethens
- Applicant: THALES
- Applicant Address: FR Courbevoie
- Assignee: Thales
- Current Assignee: Thales
- Current Assignee Address: FR Courbevoie
- Agency: Davis Wright Tremaine LLP
- Agent Michael J. Donohue
- Priority: FR1201028 20120406
- Main IPC: G06F19/00
- IPC: G06F19/00 ; G01S19/39 ; G01S19/15 ; G01S19/20 ; G01C21/16 ; G01C21/20 ; G05D1/04

Abstract:
Device for receiving radio-navigation signals, for aiding the piloting of an aircraft, comprising a first master GNSS module and a second slave GNSS module which are dissimilar, the first master GNSS module comprising a first means for processing radio-navigation signals and a first means for computing guidance data (Xg), the second slave GNSS module comprising a second means for processing radio-navigation signals and a second means for computing guidance data (Xg) on the basis of the measurements provided by the said second means for processing signals, each GNSS module furthermore comprising a comparison means for comparing between the outputs Xg1,Xg2 of the said first and second means for computing guidance data, suitable for executing the following integrity test: |Xg1−Xg2|>Kg·√{square root over (Variance(Xg1−Xg2))} and for inferring an integrity defect if the said integrity test is satisfied.
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