Analysis of Laser Gyro Strap-down Inertial Navigation System for its Self-Navigation and Integrated-Navigation Experiments in the Static State

DOI

10.2991/icmmct-16.2016.5How to use a DOI?

Keywords

Laser gyro strap-down inertia navigation system; integrated navigation; self-navigation; the static state.

Abstract

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 11.16″, 3.52″, 2.08″, 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 15.17″, 3.74″, 5.22″, 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.

Copyright

© 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/).

Download article (PDF)

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  -