发明名称 Integrity monitoring method for GNSS navigation based on historical information
摘要 The invention relates to a method of estimating the clock-position of a GNSS receiver based on pseudorange measurements Á i of a group of epochs i of measurement, i =1,..., N , where M ¡ is the number of pseudorange measurements in the epoch i ; the method comprises: - constructing a floating path from change of state estimations V i between successive epochs which are provided as input by a change of state estimation algorithm; - determining an anchor point for said path by anchor point for said path by an iterative least squares process estimating the state vector S 1 of the receiver in a preestablished anchor epoch within the measurement epochs of the path, said least squares process being carried out by means of a valid observation matrix H for the N epochs defining said floating path, said observation matrix H being constructed by juxtaposing the observation matrices H i associated to different epochs i =1,..., N , wherein each observation matrix H i is a four-column matrix the rows of which are the line of sight unit vectors of the different satellites in sight in the epoch i , juxtaposed with a 1 associated to the receiver clock component.
申请公布号 EP2037291(A1) 申请公布日期 2009.03.18
申请号 EP20070380249 申请日期 2007.09.11
申请人 GMV AEROSPACE AND DEFENCE S.A. 发明人 AZAOLA SAENZ, MIGUEL;LOPEZ ALMANSA, JOSE MARIA
分类号 G01S5/14;G01S19/20;G01S19/42 主分类号 G01S5/14
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