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1.发明授权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公开(公告)号：US09395446B2
公开(公告)日：2016-07-19
申请号：US13855430
申请日：2013-04-02
Applicant: THALES
Inventor： Stephane Rollet , Jean-Pierre Arethens
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.
Abstract translation: 用于接收无线电导航信号的装置，用于辅助飞行员的驾驶，包括不相似的第一主GNSS模块和第二从属GNSS模块，所述第一主GNSS模块包括用于处理无线电导航信号的第一装置和第一 用于计算引导数据（Xg）的装置，所述第二从属GNSS模块包括用于处理无线电导航信号的第二装置和用于根据由所述第二装置处理信号提供的测量来计算引导数据（Xg）的第二装置 每个GNSS模块还包括比较装置，用于比较用于计算引导数据的所述第一和第二装置的输出Xg1，Xg2，适用于执行以下完整性测试：| Xg1-Xg2 |> Kg·√{平方根 （方差（Xg1-Xg2））}，并且如果满足所述完整性测试则推断完整性缺陷。
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2.发明申请ONBOARD AIRCRAFT LANDING SYSTEM, BASED ON A GNSS SYSTEM, WITH REDUNDANT AND DISSIMILAR ARCHITECTURE FOR HIGH INTEGRITY LEVEL 有权基于全球导航卫星系统的ONBOARD飞机着陆系统，具有高度一致性的冗余和分辨率结构公开(公告)号：US20150362598A1
公开(公告)日：2015-12-17
申请号：US13855430
申请日：2013-04-02
Applicant: THALES
Inventor： Stephane Rollet , Jean-Pierre Arethens
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.
Abstract translation: 用于接收无线电导航信号的装置，用于辅助飞行员的驾驶，包括不相似的第一主GNSS模块和第二从属GNSS模块，所述第一主GNSS模块包括用于处理无线电导航信号的第一装置和第一 用于计算引导数据（Xg）的装置，所述第二从属GNSS模块包括用于处理无线电导航信号的第二装置和用于根据由所述第二装置处理信号提供的测量来计算引导数据（Xg）的第二装置 每个GNSS模块还包括比较装置，用于比较用于计算引导数据的所述第一和第二装置的输出Xg1，Xg2，适用于执行以下完整性测试：| Xg1-Xg2 |> Kg·√{平方根 （方差（Xg1-Xg2））}，并且如果满足所述完整性测试则推断完整性缺陷。
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