@inproceedings{a32c1de06ec9457e83bb87ee73adec24,
title = "Attitude determination of extended Kalman filtering based on quaternion",
abstract = "An extended Kalman filtering technique for the large angular maneuvering and normal mode attitude determination of a satellite is presented by using gyro, sun sensors and infrared horizon scanners. The attitude quaternion representation is adapted to design an attitude estimator and integration linear error equations are established. The results of the simulation show that attitude determination is accurately achieved by using the attitude determination algorithm.",
keywords = "Attitude determination, Attitude quaternion, Extended Kalman filtering, Satellite",
author = "Li, {Jin Iiang} and Liu, {Xiang Dong} and Zhang, {Yu He} and Xiu, {Chun Bo}",
year = "2004",
language = "English",
isbn = "7810545000",
series = "Proceedings of the 2004 Chinese Control and Decision Conference (16thCDC)",
pages = "295--298",
editor = "J.-Y. Yang and H.-W. Cao and J.-L. Li and Y.-H. Sun and Y.-Q. Chang",
booktitle = "Proceedings of the 2004 Chinese Control and Decision Conference (16th CDC)",
note = "Proceedings of the 2004 Chinese Control and Decision Conference (16thCDC) ; Conference date: 29-05-2004 Through 01-06-2004",
}