Application of Attitude Matrix Row Element Sum Matching in Transfer Alignment

Article Preview

Abstract:

To reduce the calculation brought by attitude angle and attitude matrix matching as well as to insure the transfer alignment accuracy, the paper gives a method that uses slave inertial navigation system (SINS) error model as the state-space model. The complexity of the state equation can be simplified by this method, for the lever-arm effect can be compensated in the observables rather than considering it in the equation of state, in which the inputs do not need to be brought in the equation of state; On the basis of element matching of the attitude matrix with SINS and master inertial navigation system (MINS), the paper raises row elements sum matching method of attitude matrix, which has simpler structure of the observation matrix and lower dimension compared to attitude angle matching and element matching of the attitude matrix, so as to decrease filtering computation. Simulation results have proved that the model and matching algorithm in this paper are effective and the system can achieve higher transfer alignment accuracy.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

506-512

Citation:

Online since:

July 2013

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2013 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Yongyuan Qin: Inertial Navigation Systems (Science Publications, Beijing 2005, in Chinese)

Google Scholar

[2] Xin Qi, Qinsu Peng and Changshan Zhao: Journal of Astronautics Vol. 32-1 (2011), pp.81-87(in Chinese)

Google Scholar

[3] C Yang, C F Lin and D Tarrant: Transfer alignment design and evaluation. AIAA Guidance, Navigation and Control Conference, Monterey, CA; US; 9-11 Aug. 1993. P. 1724-1733.

DOI: 10.2514/6.1993-3892

Google Scholar

[4] Qingwei Gao, Guorong Zhao and Xibin Wang: Acta Aeronautica Et Astronautica Sinica Vol. 30-11 (2009), pp.2172-2177 (in Chinese)

Google Scholar

[5] Ziwei Guo, Lingjuan Miao and Jun Shen: Journal of Astronautics Vol. 32-11 (2011), pp.2357-2364 (in Chinese)

Google Scholar

[6] J E Kain, J R Cloutier: Rapid Transfer Alignment for Tactical Weapon Application, Journal of Astronautics, The AIAA Guidance, Navigation, and Control Conference, Boston, USA, Aug 14-16, 1989.

DOI: 10.2514/6.1989-3581

Google Scholar

[7] Yinghong Han, Wanchun Chen: Journal of Beijing University of Aeronautics and Astronautics Vol. 38-2 (2012), pp.149-152 (in Chinese)

Google Scholar

[8] Jiahe Xia, Yongyuan Qin and Jinchuan You: Journal of Beijing University of Aeronautics and Astronautics Vol. 31-2(2010), pp.410-415(in Chinese)

Google Scholar

[9] Gongmin Yan, Weisheng Yan and Demin Xu: Journal of Chinese Inertial Technology Vol. 16-3 (2008), pp.253-264(in Chinese)

Google Scholar

[10] G C Li, Q T Zhang and Y B Gao: Transfer Alignment Algorithm Based on Attitude Information, IEEE Intelligent Computation Technology and Automation, Changsha, China, May 11-12, 2010.

Google Scholar

[11] Kai Chen, Hao Lu and Jie Yan: Acta Aeronautica Et Astronautica Sinica Vol. 29-4 (2008), pp.981-987(in Chinese)

Google Scholar