An attitude measurement method to compensate the error of algorithm precision based on three-axis gyroscope
Yixiang Shi, Ke Chen, Deyi Chen
Available Online June 2017.
- https://doi.org/10.2991/gcmce-17.2017.8How to use a DOI?
- Attitude measurement, Angular-rate integral, Error compensation
- In order to compensate the error of angular-rate integral and improve the precision when it comes to measure the attitude of carrier , a method based on 3-axis gyroscope is proposed. The movement of carrier is viewed as time series based on sampling interval, and two adjacent measurements are relative. The difference between two adjacent measurements will reveal the trend of angular rate, which can be used to adjust the angular rate and correct the measurements of gyroscope to compensate the error of algorithm. Experiment results show that the proposed method can get a more accurate attitude information of carrier through compensation and the simulation in different sampling frequencies are consistent.
- Open Access
- This is an open access article distributed under the CC BY-NC license.
Cite this article
TY - CONF AU - Yixiang Shi AU - Ke Chen AU - Deyi Chen PY - 2017/06 DA - 2017/06 TI - An attitude measurement method to compensate the error of algorithm precision based on three-axis gyroscope BT - 2017 Global Conference on Mechanics and Civil Engineering (GCMCE 2017) PB - Atlantis Press SP - 36 EP - 41 SN - 2352-5401 UR - https://doi.org/10.2991/gcmce-17.2017.8 DO - https://doi.org/10.2991/gcmce-17.2017.8 ID - Shi2017/06 ER -