Self-alignment algorithm for strapdown inertial navigation system under strong flurry interference
- 10.2991/isccca.2013.39How to use a DOI?
- inertial navigation system, interference, self-alignment, strong flurry
For the strong flurry interrupting, the body will suffer large swaying motion when it is in erecting state ,the output of its strapdown inertial navigation system (SINS) will be disturbed for the high gravitational center of IMU, the conventional methods are difficult to achieve alignment rapidly and accurately, to solve this problem, an anti-interference self-alignment algorithm for SINS which under strong flurry is presented, which utilizes the continuous attitude update in inertial reference frame to record the attitude changes caused by sway interrupt to remove the angular interrupting, and uses the characteristics that the body exists a shake center whose speed is zero to remove the linear movement interrupting by acquiring the equivalent specific force of the shake center, and then uses the estimation of the initial attitude to determinate the attitude of the body. The simulation result show that the presented algorithm can accomplish alignment quickly even in the presence of strong flurry interference without coarse alignment phase.
- © 2013, 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 - Yuegang Wang AU - Jiasheng Yang PY - 2013/02 DA - 2013/02 TI - Self-alignment algorithm for strapdown inertial navigation system under strong flurry interference BT - Proceedings of the 2nd International Symposium on Computer, Communication, Control and Automation (ISCCCA 2013) PB - Atlantis Press SP - 156 EP - 159 SN - 1951-6851 UR - https://doi.org/10.2991/isccca.2013.39 DO - 10.2991/isccca.2013.39 ID - Wang2013/02 ER -