@inproceedings{a2d976eea8324f6ba839b06847473c64,
title = "An attitude determination system of quad-rotor aircraft based on extended kalman filter and data fusion technique",
abstract = "An attitude determination system composed of gyroscopes, accelerometer and magnetometer is designed. An extended Kalman filter was used for estimating aircraft's state. The attitude can be determined via data fusion technique. The experimental results indicate that this combination could effectively restrain attitude error arising from the random drift of sensors. The system has the characteristics of small size, low cost and good reliability.",
keywords = "attitude, data fusion, extended Kalman filter",
author = "Xinfu Ye and Lian Zhu and Sun Changyin and Wei Wang",
year = "2013",
doi = "10.1007/978-3-642-42057-3\_96",
language = "英语",
isbn = "9783642420566",
series = "Lecture Notes in Computer Science (including subseries Lecture Notes in Artificial Intelligence and Lecture Notes in Bioinformatics)",
publisher = "Springer Verlag",
pages = "764--770",
booktitle = "Intelligence Science and Big Data Engineering - 4th International Conference, IScIDE 2013, Revised Selected Papers",
note = "4th International Conference on Intelligence Science and Big Data Engineering, IScIDE 2013 ; Conference date: 31-07-2013 Through 02-08-2013",
}