[an error occurred while processing this directive]
   
 
���¿��ټ��� �߼�����
   ��ҳ  �ڿ�����  ��ί��  Ͷ��ָ��  �ڿ�����  ��������  �� �� ��  ��ϵ����
�������պ����ѧѧ�� 2010, Vol. 36 Issue (7) :762-766    DOI:
���� ����Ŀ¼ | ����Ŀ¼ | ������� | �߼����� << | >>
��Ԫ��UKF��������ϵ����˲�����
Ԭ����, ����*
���������̴�ѧ �Զ���ѧԺ, ������ 150001
Quaternion unscented Kalman filtering for ultra-tight integration
Yuan Gannan, Zhang Tao*
College of Automation, Harbin Engineering University, Harbin 150001, China

ժҪ
�����
�������
Download: PDF (446KB)   HTML 1KB   Export: BibTeX or EndNote (RIS)      Supporting Info
ժҪ ���GPS/SINS(Global Positioning System/Strapdown Inertial Navigation System)��������ϵ���ϵͳ���Ի��˲��ڸ߶�̬����GPS�źŵȻ����������½����ص�����,�����һ������Ԫ��UKF(Unscented Kalman Filter)Ϊ������GPS/SINS��������ϵ���ϵͳ�������˲�����.ͨ������GPS��SINS�ڳ�������ϵ���ϵͳ�еĹ�ϵ,�����һ������SINS��Ϣ�����ơ�����GPS�ز��źŵķ���,�ڴ˻����Ͻ�������ϵ����˲���״̬���̺����ⷽ��;����Ԫ���������ģ��Ϊ����,�����һ�ֿ�Ӧ����UKF�˲��������Ԫ����Ȩ��ֵ�ķ���;����˻�����Ԫ��UKF��GPS/SINS��������ϵ����˲�����.����ʵ�����:�ڸ߶�̬������,��Ԫ��UKF�˲�������ǿ��GPS/SINS��������ϵ���ϵͳ�Ķ�λ���ȺͿ���������.
Service
�ѱ����Ƽ�������
�����ҵ����
�������ù�����
Email Alert
RSS
�����������
�ؼ����� �������˲�   ����   ������ϵͳ   ���   ����ϵͳ   ȫ��λϵͳ     
Abstract�� Concerning the problem of the ultra-tightly coupled global positioning system/strapdown inertial navigation system (GPS/SINS) degraded in high dynamic and weak signal environments for linear filter, a quaternion unscented Kalman filter method was proposed. Firstly, analyzing the relationship between GPS and SINS of the ultra-tightly coupled GPS/SINS navigation system, an algorithm that using the SINS to estimate and correct the carrier signal of the GPS was derived, then the state and measurement equations was built. Secondly, concerning the problems of singularity and frequent parameter transformation for Rodrigus method, based on the multiplicative quaternion error model, a weighted averaging quaternion method that using the quaternion directly was proposed. Finally, the quaternion unscented Kalman filter method was proposed for the ultra-tightly coupled GPS/SINS navigation system. The simulation results indicate that the quaternion unsecured Kalman filter method is more robust to jamming and increases the position accuracy in high dynamic.
Keywords�� Kalman filtering   jamming   nonlinear system   integration   navigation system   global positioning system     
Received 2009-05-19;
Fund:

������Ȼ��ѧ����������Ŀ(60604019)

About author: Ԭ����(1945-),��,��������������,����,redbaronzt@hotmail.com.
���ñ���:   
Ԭ����, ����.��Ԫ��UKF��������ϵ����˲�����[J]  �������պ����ѧѧ��, 2010,V36(7): 762-766
Yuan Gannan, Zhang Tao.Quaternion unscented Kalman filtering for ultra-tight integration[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2010,V36(7): 762-766
���ӱ���:  
http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y2010/V36/I7/762
Copyright 2010 by �������պ����ѧѧ��