SINS/CNS/GNSS integrated navigation scheme for advanced upper stage

Hua Zong; Zhun Liu; Xiaoying Gao; Bo Wang; Sen Wang; Da Xu

doi:10.1109/ICMC.2014.7231938

SINS/CNS/GNSS integrated navigation scheme for advanced upper stage

Hua Zong, Zhun Liu, Xiaoying Gao, Bo Wang, Sen Wang, Da Xu

School of Automation

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

2 Citations (Scopus)

Abstract

A SINS/CNS/GNSS integrated navigation scheme is researched for advanced upper stage in this paper. First of all, the composition of the integrated navigation is introduced. Then, the error model of the integration system in launch inertial frame was established. especially the misalignments of star tracker are inputted as system states, and also the federated filter algorithm is used to estimate the state errors of the integrated navigation system. Finally, simulations results show that the SINS/CNS/GNSS integrated navigation can provide navigation parameters with high accuracy, which can meet the accuracy requirements of advanced upper stage.

Original language	English
Title of host publication	Proceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	2109-2113
Number of pages	5
ISBN (Electronic)	9781479925384
DOIs	https://doi.org/10.1109/ICMC.2014.7231938
Publication status	Published - 31 Aug 2015
Event	International Conference on Mechatronics and Control, ICMC 2014 - Jinzhou, China Duration: 3 Jul 2014 → 5 Jul 2014

Publication series

Name	Proceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014

Conference

Conference	International Conference on Mechatronics and Control, ICMC 2014
Country/Territory	China
City	Jinzhou
Period	3/07/14 → 5/07/14

Keywords

Federated filter
Integrated Navigation
launch inertial frame

Access to Document

10.1109/ICMC.2014.7231938

Cite this

Zong, H., Liu, Z., Gao, X., Wang, B., Wang, S., & Xu, D. (2015). SINS/CNS/GNSS integrated navigation scheme for advanced upper stage. In Proceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014 (pp. 2109-2113). Article 7231938 (Proceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICMC.2014.7231938

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title = "SINS/CNS/GNSS integrated navigation scheme for advanced upper stage",

abstract = "A SINS/CNS/GNSS integrated navigation scheme is researched for advanced upper stage in this paper. First of all, the composition of the integrated navigation is introduced. Then, the error model of the integration system in launch inertial frame was established. especially the misalignments of star tracker are inputted as system states, and also the federated filter algorithm is used to estimate the state errors of the integrated navigation system. Finally, simulations results show that the SINS/CNS/GNSS integrated navigation can provide navigation parameters with high accuracy, which can meet the accuracy requirements of advanced upper stage.",

keywords = "Federated filter, Integrated Navigation, launch inertial frame",

author = "Hua Zong and Zhun Liu and Xiaoying Gao and Bo Wang and Sen Wang and Da Xu",

note = "Publisher Copyright: {\textcopyright} 2014 IEEE.; International Conference on Mechatronics and Control, ICMC 2014 ; Conference date: 03-07-2014 Through 05-07-2014",

year = "2015",

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doi = "10.1109/ICMC.2014.7231938",

language = "English",

series = "Proceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

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booktitle = "Proceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014",

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Zong, H, Liu, Z, Gao, X, Wang, B, Wang, S & Xu, D 2015, SINS/CNS/GNSS integrated navigation scheme for advanced upper stage. in Proceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014., 7231938, Proceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014, Institute of Electrical and Electronics Engineers Inc., pp. 2109-2113, International Conference on Mechatronics and Control, ICMC 2014, Jinzhou, China, 3/07/14. https://doi.org/10.1109/ICMC.2014.7231938

SINS/CNS/GNSS integrated navigation scheme for advanced upper stage. / Zong, Hua; Liu, Zhun; Gao, Xiaoying et al.
Proceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014. Institute of Electrical and Electronics Engineers Inc., 2015. p. 2109-2113 7231938 (Proceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014).

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

TY - GEN

T1 - SINS/CNS/GNSS integrated navigation scheme for advanced upper stage

AU - Zong, Hua

AU - Liu, Zhun

AU - Gao, Xiaoying

AU - Wang, Bo

AU - Wang, Sen

AU - Xu, Da

PY - 2015/8/31

Y1 - 2015/8/31

N2 - A SINS/CNS/GNSS integrated navigation scheme is researched for advanced upper stage in this paper. First of all, the composition of the integrated navigation is introduced. Then, the error model of the integration system in launch inertial frame was established. especially the misalignments of star tracker are inputted as system states, and also the federated filter algorithm is used to estimate the state errors of the integrated navigation system. Finally, simulations results show that the SINS/CNS/GNSS integrated navigation can provide navigation parameters with high accuracy, which can meet the accuracy requirements of advanced upper stage.

AB - A SINS/CNS/GNSS integrated navigation scheme is researched for advanced upper stage in this paper. First of all, the composition of the integrated navigation is introduced. Then, the error model of the integration system in launch inertial frame was established. especially the misalignments of star tracker are inputted as system states, and also the federated filter algorithm is used to estimate the state errors of the integrated navigation system. Finally, simulations results show that the SINS/CNS/GNSS integrated navigation can provide navigation parameters with high accuracy, which can meet the accuracy requirements of advanced upper stage.

KW - Federated filter

KW - Integrated Navigation

KW - launch inertial frame

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U2 - 10.1109/ICMC.2014.7231938

DO - 10.1109/ICMC.2014.7231938

M3 - Conference contribution

AN - SCOPUS:84953807100

T3 - Proceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014

SP - 2109

EP - 2113

BT - Proceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - International Conference on Mechatronics and Control, ICMC 2014

Y2 - 3 July 2014 through 5 July 2014

ER -

Zong H, Liu Z, Gao X, Wang B, Wang S, Xu D. SINS/CNS/GNSS integrated navigation scheme for advanced upper stage. In Proceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014. Institute of Electrical and Electronics Engineers Inc. 2015. p. 2109-2113. 7231938. (Proceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014). doi: 10.1109/ICMC.2014.7231938

SINS/CNS/GNSS integrated navigation scheme for advanced upper stage

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