DocumentCode
2984273
Title
The Modeling and Analysis for Autonomous Navigation System Based on Tightly Coupled GPS/INS
Author
Lijun, Wang ; Xiaoniu, Yang ; Huichang, Zhao
Author_Institution
CETC, Jiaxing
fYear
2007
fDate
18-21 April 2007
Firstpage
1
Lastpage
4
Abstract
GPS can provide both military and private users with accurate information about user position and velocity. However its data rate is low as well as 1~10Hz, and it will not provide a continuous and reliable information among mountains, dense forests and high building. Inertial Navigation System (INS) is an autonomous, all-weather navigation system that can provide continuous information of position, velocity and attitude regardless of the surrounding. But the performance of INS deteriorates with time due to inertial sensor performance. GPS and INS have complementary properties, whose integration is an efficient way of improving the whole performance of navigation system. In this paper, the models of GPS and INS, respectively, are built and analyzed, and then a tightly coupled GPS/INS system based on the information of GPS position and velocity is modeled and simulated, which is compared with integrated system using only GPS position data. The simulation and analysis results demonstrate that integrated system can greatly enhance the robustness and reliability of autonomous navigation system.
Keywords
Global Positioning System; inertial navigation; sensors; GPS; autonomous navigation system; inertial navigation system; inertial sensor; Accelerometers; Analytical models; Coupled mode analysis; Differential equations; Filters; Global Positioning System; Inertial navigation; Position measurement; Satellites; Velocity measurement;
fLanguage
English
Publisher
ieee
Conference_Titel
Microwave and Millimeter Wave Technology, 2007. ICMMT '07. International Conference on
Conference_Location
Builin
Print_ISBN
1-4244-1049-5
Electronic_ISBN
1-4244-1049-5
Type
conf
DOI
10.1109/ICMMT.2007.381501
Filename
4266260
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