DocumentCode :
691054
Title :
Research on Initial Alignment of SINS for Marching Vehicle
Author :
Nie Qi
Author_Institution :
Beijing Aerosp. Autom. Control Inst., Beijing, China
fYear :
2013
fDate :
21-23 Sept. 2013
Firstpage :
465
Lastpage :
468
Abstract :
Standard extended Kalman filtering algorithm usually needs a little precise initial value, but Strap down inertial navigation system(SINS) coarse alignment precision for marching vehicle can´t meet the requirement. So UKF (unscented kalman filter) was proposed to achieve SINS initial alignment for marching vehicle with odometer aiding. The state equation for large misalignment error model was expounded, and observation equation was derived when the measurement variable was chosen as difference of velocity offered by SINS and velocity reckoned by odometer. UKF filtering algorithm based on additive noise model was derived. Simulation based on vehicular tests data showed that UKF filtering algorithm could achieve SINS initial alignment for marching vehicle, and UKF filtering algorithm could achieve better robustness from filtering initial value, higher alignment precision and faster convergence velocity than Standard extended Kalman filtering algorithm.
Keywords :
Kalman filters; accelerometers; distance measurement; gyroscopes; inertial navigation; nonlinear filters; SINS initial alignment; additive noise model; coarse alignment precision; large misalignment error model; marching vehicle; odometer aid; strapdown inertial navigation system; unscented Kalman filter; velocity reckoning; Convergence; Equations; Kalman filters; Mathematical model; Navigation; Silicon compounds; Vehicles; UKF filtering algorithm; error model for large misalignment; initial alignment of SINS;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Instrumentation, Measurement, Computer, Communication and Control (IMCCC), 2013 Third International Conference on
Conference_Location :
Shenyang
Type :
conf
DOI :
10.1109/IMCCC.2013.106
Filename :
6840496
Link To Document :
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