Robust INS/SFPPP-BDS tightly coupled navigation algorithm with adaptive cycle slip compensation model

被引:0
|
作者
Ma, Hangshuai [1 ,2 ]
Wang, Rong [3 ]
Xiong, Zhi [3 ]
Liu, Jianye [3 ]
Li, Chuanyi [3 ]
机构
[1] Sci & Technol Avion Integrat Lab, Shanghai, Peoples R China
[2] China Natl Aeronaut Radio Elect Res Inst, Shanghai, Peoples R China
[3] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nav Res Ctr, Nanjing 211106, Jiangsu, Peoples R China
关键词
Integrated navigation; tightly coupled IN; BDS integration; single-frequency precise point positioning; cycle slip compensation model; robust fusion; PPP; GPS; INS;
D O I
10.1177/1748301819833044
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
The application of Beidou Satellite Navigation System (BDS) is developing rapidly. To satisfy the increasing demand for positioning performance, single-frequency precise point positioning (SFPPP) has been a focus in recent years. By introducing the SFPPP technique into the INS/BDS integrated system, higher navigation accuracy can be obtained. Cycle slip, which is caused by signal blockage during the measurement of the carrier phase, is a challenge for SFPPP application. In the INS/SFPPP-BDS integrated system, cycle slip can cause serious bias in BDS carrier phase measurements. In this paper, a new INS/SFBDS-PPP tightly coupled navigation system and a robust adaptive filtering method are proposed. Using a low-cost single-frequency receiver integrated with INS, an observation model was built based on the pseudo range and carrier phase by PPP preprocessing. The cycle slip was introduced into the state vector to improve the estimation precision. The test statistics, comprising the innovation and its covariance, were used to estimate the time at which cycle slip occurred and its amplitude to compensate for its effect on the observation. Finally, the proposed system model and algorithm are validated by simulation.
引用
收藏
页码:1 / 11
页数:11
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