Development of the dual-frequency dual-constellation airborne multipath models

被引:11
作者
Circiu, Mihaela-Simona [1 ,2 ]
Caizzone, Stefano [1 ]
Felux, Michael [1 ]
Enneking, Christoph [1 ]
Rippl, Markus [1 ]
Meurer, Michael [1 ,2 ]
机构
[1] German Aerosp Ctr DLR, Inst Commun & Nav, D-82234 Wessling, Germany
[2] Rhein Westfal TH Aachen, D-52074 Aachen, Germany
来源
NAVIGATION-JOURNAL OF THE INSTITUTE OF NAVIGATION | 2020年 / 67卷 / 01期
关键词
This paper presents a methodology to build multipath models for aviation use of new Global Positioning System (GPS) and Galileo signals. The estimation of airframe multipath errors makes use of carrier phase measurements; thus; it is affected by the integer ambiguities. A new method for removing the ambiguities from the multipath estimation is presented. The method is suitable for measurements from flight data and is able to exclude measurements highly affected by multipath from the estimation by using a derived standard deviation based on the receiver thermal noise only. Next; an overview of the error sources relevant for the multipath estimation is given; and a first concept to separate the receiver antenna errors from the multipath errors is proposed. Finally; the paper discusses overbounding of the observed multipath errors to safely bound the tail risks and the inflation needed to account for uncertainty due to limited amounts of data. © 2020 The Authors. Navigation published by Wiley Periodicals; Inc. on behalf of Institute of Navigation;
D O I
10.1002/navi.344
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper presents a methodology to build multipath models for aviation use of new Global Positioning System (GPS) and Galileo signals. The estimation of airframe multipath errors makes use of carrier phase measurements; thus, it is affected by the integer ambiguities. A new method for removing the ambiguities from the multipath estimation is presented. The method is suitable for measurements from flight data and is able to exclude measurements highly affected by multipath from the estimation by using a derived standard deviation based on the receiver thermal noise only. Next, an overview of the error sources relevant for the multipath estimation is given, and a first concept to separate the receiver antenna errors from the multipath errors is proposed. Finally, the paper discusses overbounding of the observed multipath errors to safely bound the tail risks and the inflation needed to account for uncertainty due to limited amounts of data.
引用
收藏
页码:61 / 81
页数:21
相关论文
共 18 条
[1]  
[Anonymous], 2004, ISGPS200D
[2]  
[Anonymous], 2013, ED114A EUR
[3]  
[Anonymous], 2018, DO373
[4]  
[Anonymous], 2018, ED259
[5]  
[Anonymous], 2017, UNDERSTANDING GPS PR
[6]  
Booth J, 2000, P IAIN WORLD C 56 AN, P689
[7]  
Caizzone S, 2017, I NAVIG SAT DIV INT, P3460
[8]   Antenna influence on Global Navigation Satellite System pseudorange performance for future aeronautics multifrequency standardization [J].
Caizzone, Stefano ;
Circiu, Mihaela-Simona ;
Elmarissi, Wahid ;
Enneking, Christoph ;
Felux, Michael ;
Yinusa, Kazeem .
NAVIGATION-JOURNAL OF THE INSTITUTE OF NAVIGATION, 2019, 66 (01) :99-116
[9]  
Harris M, 2017, P INT TECH M I NAVIG, P591
[10]  
Hatch R.R., 1982, PROC 3 INT GEODETIC, P1213