Title :
An integrated system of GPS and INS with azimuth rotated platform
Author :
Wang Rong-ying ; Xu Jiang-ning ; Bian Hong-wei
Author_Institution :
Navig. Eng. Dept., Navy Univ. of Eng., Wuhan, China
Abstract :
For its synergistic relationship, the integrated GPS/INS navigation system has been adopted in many navigation systems. The azimuth rotating Gimbaled Inertial Navigation system (ARGINS) can modulate the gyro drift and accelerometer bias by rotating the platform about the azimuth axis and so improve the observability properties of errors and the navigation accuracy. In this paper, the dynamic error model and the measurement model of loosely integrated ARGINS/GPS system for kalman filter are derived first,then the simulation is carried out for integrated ARGINS/GPS system, which adopts the position and velocity as its measurement variables. The simulation result shows that the ARGINS/GPS system can improve the evaluation precision and the quickness of horizontal misalignment angles of platform, compared with the integrated system of north-pointing GINS and GPS.
Keywords :
Global Positioning System; Kalman filters; inertial navigation; Kalman filter; accelerometer bias; azimuth axis; azimuth rotated platform; azimuth rotating Gimbaled inertial navigation system; dynamic error model; gyro drift; integrated GPS/INS navigation system; measurement model; synergistic relationship; Azimuth; Global Positioning System; Sensors; Azimuth Rotating GINS; GPS; Integrated Navigation System; Kalman filtering;
Conference_Titel :
Computer Application and System Modeling (ICCASM), 2010 International Conference on
Conference_Location :
Taiyuan
Print_ISBN :
978-1-4244-7235-2
Electronic_ISBN :
978-1-4244-7237-6
DOI :
10.1109/ICCASM.2010.5620497