[an error occurred while processing this directive]
   
 
���¿��ټ��� �߼�����
   ��ҳ  �ڿ�����  ��ί��  Ͷ��ָ��  �ڿ�����  ��������  �� �� ��  ��ϵ����
�������պ����ѧѧ�� 2009, Vol. 35 Issue (6) :728-731    DOI:
���� ����Ŀ¼ | ����Ŀ¼ | ������� | �߼����� << | >>
ҡ�ڻ���SINS���پ�ȷ���ݶ�׼����
������, ������, �� ��*
�������պ����ѧ �ѧԺ, ���� 100191
Transfer alignment of strapdown inertial navigation systems on rolling bases
Wang Xinlong, Shen Liangliang, Ma Shan*
School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

ժҪ
�����
�������
Download: PDF (0KB)   HTML 1KB   Export: BibTeX or EndNote (RIS)      Supporting Info
ժҪ ��������׼ʱ,ϵͳģ�͵ľ�ȷ�Լ�״̬�Ŀɹ۲��ԺͿɹ۲���Ǿ�����̬ϵͳ�������˲�Ч������Ҫ����.�����˿�����-�ӹߵ�ƥ����Ϣʱ���ӳ������ҡ�ڻ��������ߵ�ϵͳSINS(Strapdown Inertial Naviagtion System)��ȷ���ݶ�׼ģ��,��PWCS(Piece-Wise Constant System)�ɹ۲���������ֵ�ֽ�ɹ۲�ȷ�����������,�Ի����ڲ�ͬҡ�ڷ�ʽ�½�������SINS״̬�Ŀɹ۲�Ƚ����˶�������,�õ��˻���������ҡ���˶�ʱSINS��״̬����������ѵĿɹ�������,�Ӷ�ʹSINS�ɻ�����ŵĶ�׼�ٶȺ;���.�÷���Ϊ����������ʼ��׼ʱ������ѻ������������ݶ�׼ƥ��ģʽ��ѡ���ṩ������,�����������˸÷�������ȷ�Ժ���Ч��.
Service
�ѱ����Ƽ�������
�����ҵ����
�������ù�����
Email Alert
RSS
�����������
������
������
����
�ؼ����� ���Ե���ϵͳ   ��׼   ʱ�����   �ɹ۲���   �������˲�     
Abstract�� In the process of initial alignment for rolling bases, the accuracy of a model and the observability and observability degree of states are important facts to confirm the filtering effect. A fast and precise alignment method for rolling bases was discussed. Considering time-delay between the master and slave inertial navigation system, a precise transfer alignment model of "velocity + pose" matching was established. The observability analysis of piece-wise constant system (PWCS) and singular value decomposition of observability degree were combined, the observability degree of strapdown inertial navigation system (SINS) -s states were analyzed quantificationally, and the optimal estimation of SINS can be received at the three axes rolling state. Consequently, the SINS can achieve the optimal speed and precision of initial alignment performance. The choice of optimal maneuvers trajectory for carriers and the matching mode of transfer alignment can be gained for alignment of carrier weapons. The simulation results validate the efficiency of this method.
Keywords�� inertial navigation system   alignment   time measurement   observability   Kalman filtering     
Received 2008-04-04;
Fund:

ˮ����Ϣ��������ƹ����Ƽ��ص�ʵ���һ���������Ŀ(51448020105HK0101); �������պ����ѧ�̸�������Ŀ(2008)

About author: ������(1969��),��,�������,������,xlwon@163.com.
���ñ���:   
������, ������, �� ��.ҡ�ڻ���SINS���پ�ȷ���ݶ�׼����[J]  �������պ����ѧѧ��, 2009,V35(6): 728-731
Wang Xinlong, Shen Liangliang, Ma Shan.Transfer alignment of strapdown inertial navigation systems on rolling bases[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2009,V35(6): 728-731
���ӱ���:  
http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y2009/V35/I6/728
Copyright 2010 by �������պ����ѧѧ��