Attitude determination of extended Kalman filtering based on quaternion

Jin Iiang Li; Xiang Dong Liu; Yu He Zhang; Chun Bo Xiu

Attitude determination of extended Kalman filtering based on quaternion

Jin Iiang Li, Xiang Dong Liu, Yu He Zhang, Chun Bo Xiu

School of Automation

Beijing Institute of Technology

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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.

Original language	English
Title of host publication	Proceedings of the 2004 Chinese Control and Decision Conference (16th CDC)
Editors	J.-Y. Yang, H.-W. Cao, J.-L. Li, Y.-H. Sun, Y.-Q. Chang
Pages	295-298
Number of pages	4
Publication status	Published - 2004
Event	Proceedings of the 2004 Chinese Control and Decision Conference (16thCDC) - Huangshan, China Duration: 29 May 2004 → 1 Jun 2004

Publication series

Name	Proceedings of the 2004 Chinese Control and Decision Conference (16thCDC)

Conference

Conference	Proceedings of the 2004 Chinese Control and Decision Conference (16thCDC)
Country/Territory	China
City	Huangshan
Period	29/05/04 → 1/06/04

Keywords

Attitude determination
Attitude quaternion
Extended Kalman filtering
Satellite

Cite this

Li, Jin Iiang ; Liu, Xiang Dong ; Zhang, Yu He et al. / Attitude determination of extended Kalman filtering based on quaternion. Proceedings of the 2004 Chinese Control and Decision Conference (16th CDC). editor / J.-Y. Yang ; H.-W. Cao ; J.-L. Li ; Y.-H. Sun ; Y.-Q. Chang. 2004. pp. 295-298 (Proceedings of the 2004 Chinese Control and Decision Conference (16thCDC)).

@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",

}

Li, JI, Liu, XD, Zhang, YH & Xiu, CB 2004, Attitude determination of extended Kalman filtering based on quaternion. in J-Y Yang, H-W Cao, J-L Li, Y-H Sun & Y-Q Chang (eds), Proceedings of the 2004 Chinese Control and Decision Conference (16th CDC). Proceedings of the 2004 Chinese Control and Decision Conference (16thCDC), pp. 295-298, Proceedings of the 2004 Chinese Control and Decision Conference (16thCDC), Huangshan, China, 29/05/04.

Attitude determination of extended Kalman filtering based on quaternion. / Li, Jin Iiang; Liu, Xiang Dong; Zhang, Yu He et al.
Proceedings of the 2004 Chinese Control and Decision Conference (16th CDC). ed. / J.-Y. Yang; H.-W. Cao; J.-L. Li; Y.-H. Sun; Y.-Q. Chang. 2004. p. 295-298 (Proceedings of the 2004 Chinese Control and Decision Conference (16thCDC)).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Attitude determination of extended Kalman filtering based on quaternion

AU - Li, Jin Iiang

AU - Liu, Xiang Dong

AU - Zhang, Yu He

AU - Xiu, Chun Bo

PY - 2004

Y1 - 2004

N2 - 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.

AB - 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.

KW - Attitude determination

KW - Attitude quaternion

KW - Extended Kalman filtering

KW - Satellite

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M3 - Conference contribution

AN - SCOPUS:4744339278

SN - 7810545000

T3 - Proceedings of the 2004 Chinese Control and Decision Conference (16thCDC)

SP - 295

EP - 298

BT - Proceedings of the 2004 Chinese Control and Decision Conference (16th CDC)

A2 - Yang, J.-Y.

A2 - Cao, H.-W.

A2 - Li, J.-L.

A2 - Sun, Y.-H.

A2 - Chang, Y.-Q.

T2 - Proceedings of the 2004 Chinese Control and Decision Conference (16thCDC)

Y2 - 29 May 2004 through 1 June 2004

ER -

Attitude determination of extended Kalman filtering based on quaternion

Abstract

Publication series

Conference

Keywords

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