DocumentCode :
1795266
Title :
Research on vehicle inertial navigation system dynamic correction technology based on reference object
Author :
Shenghong Xu ; Ruitao Li ; Wenjing Cao
Author_Institution :
Dept. of Control Eng., Naval Aeronaut. & Astronaut. Univ., Yantai, China
fYear :
2014
fDate :
8-10 Aug. 2014
Firstpage :
2173
Lastpage :
2176
Abstract :
The integrated system composed of inertial navigation system (INS) and speedometer is an independent positioning system commonly used on military vehicles. The INS attitude accuracy will affect the integrated location accuracy directly. This paper studied the INS error estimation and correction technique based on reference object with laser ranging information. Simulation results show that the method is an effective way to correct the vehicle INS attitude parameters during vehicle driving with ranging information, and can improve the precision of the integrated positioning system.
Keywords :
inertial navigation; laser ranging; military vehicles; INS attitude accuracy; INS correction technique; INS error estimation; independent positioning system; integrated location accuracy; integrated positioning system; laser ranging information; military vehicles; reference object; speedometer; vehicle INS attitude parameters; vehicle inertial navigation system dynamic correction technology; Distance measurement; Mathematical model; Navigation; Silicon compounds; Vectors; Vehicle dynamics; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location :
Yantai
Print_ISBN :
978-1-4799-4700-3
Type :
conf
DOI :
10.1109/CGNCC.2014.7007510
Filename :
7007510
Link To Document :
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