Analysis of Laser Gyro Strap-down Inertial Navigation System for its Self-Navigation and Integrated-Navigation Experiments in the Static State
Yun-Fei Mao, Lin Ou, Yi Zhao
Available Online March 2016.
- 10.2991/icmmct-16.2016.5How to use a DOI?
- Laser gyro strap-down inertia navigation system; integrated navigation; self-navigation; the static state.
In this paper, the test for the laser gyro strap-down inertial navigation system is studied. The self-navigation and the integrated navigation are introduced. By comparing the measuring results with the real data, the accuracy for the integrated-navigation is obtained. The errors for the head, the roll and the pitch are 11.16â€³, 3.52â€³, 2.08â€³, for the location is 0.13m. In the same way, the accuracy for the self-navigation is obtained. The errors for the head, the roll and the pitch are 15.17â€³, 3.74â€³, 5.22â€³, for the location is 0.56m. As a result, we can find that the accuracy for the integrated navigation is better than the self-navigation, however they both agree well with the designing results.
- © 2016, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
Cite this article
TY - CONF AU - Yun-Fei Mao AU - Lin Ou AU - Yi Zhao PY - 2016/03 DA - 2016/03 TI - Analysis of Laser Gyro Strap-down Inertial Navigation System for its Self-Navigation and Integrated-Navigation Experiments in the Static State BT - Proceedings of the 2016 4th International Conference on Machinery, Materials and Computing Technology PB - Atlantis Press SP - 21 EP - 24 SN - 2352-5401 UR - https://doi.org/10.2991/icmmct-16.2016.5 DO - 10.2991/icmmct-16.2016.5 ID - Mao2016/03 ER -