DATA FUSION ALGORITHM OF BARO/GPS BASED ON DELTA-ALTITUDE

被引:3
作者
Yao, Yi [1 ]
Huang, Zhi-gang [1 ]
Li, Rui [1 ]
机构
[1] Beihang Univ, Sch Elect & Informat Engn, Beijing, Peoples R China
来源
2009 IEEE YOUTH CONFERENCE ON INFORMATION, COMPUTING AND TELECOMMUNICATION, PROCEEDINGS | 2009年
关键词
Integrated Navigation; Data Fusion; Barometric Altimeter; Integrity; Accuracy;
D O I
10.1109/YCICT.2009.5382443
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
As we all know, GPS cannot totally meet the need of safety-of-life applications in civilian aviation especially the vertical accuracy and integrity. It is widely accepted that integrating GPS with barometric altimeter (Baro) can improve geometry and consequently provide performance enhancement especially in the vertical direction. This paper presents a novel data fusion algorithm of Baro and GPS based on delta-altitude. This algorithm removes some of the conservatism built into the prior positioning algorithm of Baro/GPS integrated system. This paper focuses on analysis of accuracy and integrity performance of Baro/GPS integrated system. The results of simulation show that this algorithm can substantially improves navigation accuracy performance of the integrated system, especially in the vertical direction. Meanwhile, it indicates that great enhancement is achieved in integrity performance.
引用
收藏
页码:522 / 525
页数:4
相关论文
共 7 条
[1]  
[Anonymous], 2017, UNDERSTANDING GPS PR
[2]  
JAN SS, 2008, IEEE T AERO ELEC SYS, P127
[3]  
JAN SS, 2002, P 15 INT TECHN M SAT, P2576
[4]   Analysis of pressure and blanchard altitude errors computed using atmospheric data obtained from an F-18 aircraft flight [J].
Li, TC ;
Shaner, RD .
2002 IEEE POSITION LOCATION AND NAVIGATION SYMPOSIUM, 2002, :344-350
[5]   Autonomous fault detection and removal using GPS carrier phase [J].
Pervan, BS ;
Lawrence, DG ;
Parkinson, BW .
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1998, 34 (03) :897-906
[6]  
TANG W, 2005, AEROSPACE ELECT SYST, P24
[7]  
WANG YC, 2006, THESIS BEIHANG U BEI, P11