DocumentCode :
596640
Title :
Research of Fuzzy Inference based on Simplified UKF for large alignment errors in SINS alignment on a swaying base
Author :
Weiwei Yang ; Lingjuan Miao ; Ze Guo
Author_Institution :
Sch. of Autom., Beijing Inst. of Technol., Beijing, China
fYear :
2012
fDate :
18-20 Oct. 2012
Firstpage :
539
Lastpage :
544
Abstract :
In the condition of large alignment angles which brought about nonlinear problem in SINS, a precise SINS error model was established on the concept of Euler platform error angles. To reduce the computation of initial alignment in SINS, a Simplified UKF (SUKF) could be used since its state equation was nonlinear while the measurement equation was linear. A novel method combined Fuzzy Inference System (FIS) and system noise´s online estimation together on the basis of SUKF was proposed to adjust the system noise covariance, and online improve the performance of the SINS initial alignment. In the SINS alignment for large misalignment angles simulation conditions, the SUKF via FIS showed higher accuracy, better stability and also better real-time performance compared with conventional UKF.
Keywords :
Kalman filters; aerospace computing; digital simulation; fuzzy reasoning; inertial navigation; FIS; SINS alignment; SUKF; alignment errors; fuzzy inference system; large alignment angles; misalignment angles simulation conditions; nonlinear problem; precise SINS error model; simplified UKF; swaying base; Equations; Estimation; Kalman filters; Mathematical model; Noise; Silicon compounds;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Advanced Computational Intelligence (ICACI), 2012 IEEE Fifth International Conference on
Conference_Location :
Nanjing
Print_ISBN :
978-1-4673-1743-6
Type :
conf
DOI :
10.1109/ICACI.2012.6463222
Filename :
6463222
Link To Document :
بازگشت