Unscented Kalman Filter based two-stage estimation of spacecraft position and velocity with single station antenna tracking data

Chingiz Hajiyev; Melih Ata

doi:10.1109/RAST.2015.7208445

Unscented Kalman Filter based two-stage estimation of spacecraft position and velocity with single station antenna tracking data

Chingiz Hajiyev, Melih Ata

Department of Aeronautical Engineering

Istanbul Technical University

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

Abstract

In this study, a two-stage approach for estimation of spacecraft's position and velocity by single station antenna tracking data is proposed. In the first stage, direct nonlinear antenna measurements are transformed to linear x-y-z coordinate measurements of spacecraft's position, and statistical characteristics of orbit determination errors are analyzed. Variances of orbit parameters' errors are chosen as the accuracy criteria. In the second stage, the outputs of the first stage are improved by the designed Unscented Kalman Filter (UKF) for estimation of the spacecraft's position and velocity on indirect linear x-y-z measurements. In simulations, position and velocity values of a geostationary satellite are found via proposed two-stage procedure.

Original language	English
Title of host publication	RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies
Editors	M. Fevzi Unal, Suleyman Basturk, Okyay Kaynak, Abdurrahman Hacioglu, Fuat Ince
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	777-782
Number of pages	6
ISBN (Electronic)	9781467377607
DOIs	https://doi.org/10.1109/RAST.2015.7208445
Publication status	Published - 17 Aug 2015
Event	7th International Conference on Recent Advances in Space Technologies, RAST 2015 - Istanbul, Turkey Duration: 16 Jun 2015 → 19 Jun 2015

Publication series

Name	RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies

Conference

Conference	7th International Conference on Recent Advances in Space Technologies, RAST 2015
Country/Territory	Turkey
City	Istanbul
Period	16/06/15 → 19/06/15

Bibliographical note

Publisher Copyright:
© 2015 IEEE.

Keywords

estimation
indirect measurements (key words)
single station antenna
spacecraft
Unscented Kalman filter

Access to Document

10.1109/RAST.2015.7208445

Cite this

Hajiyev, C., & Ata, M. (2015). Unscented Kalman Filter based two-stage estimation of spacecraft position and velocity with single station antenna tracking data. In M. F. Unal, S. Basturk, O. Kaynak, A. Hacioglu, & F. Ince (Eds.), RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies (pp. 777-782). Article 7208445 (RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/RAST.2015.7208445

Hajiyev, Chingiz ; Ata, Melih. / Unscented Kalman Filter based two-stage estimation of spacecraft position and velocity with single station antenna tracking data. RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies. editor / M. Fevzi Unal ; Suleyman Basturk ; Okyay Kaynak ; Abdurrahman Hacioglu ; Fuat Ince. Institute of Electrical and Electronics Engineers Inc., 2015. pp. 777-782 (RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies).

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abstract = "In this study, a two-stage approach for estimation of spacecraft's position and velocity by single station antenna tracking data is proposed. In the first stage, direct nonlinear antenna measurements are transformed to linear x-y-z coordinate measurements of spacecraft's position, and statistical characteristics of orbit determination errors are analyzed. Variances of orbit parameters' errors are chosen as the accuracy criteria. In the second stage, the outputs of the first stage are improved by the designed Unscented Kalman Filter (UKF) for estimation of the spacecraft's position and velocity on indirect linear x-y-z measurements. In simulations, position and velocity values of a geostationary satellite are found via proposed two-stage procedure.",

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year = "2015",

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doi = "10.1109/RAST.2015.7208445",

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Hajiyev, C & Ata, M 2015, Unscented Kalman Filter based two-stage estimation of spacecraft position and velocity with single station antenna tracking data. in MF Unal, S Basturk, O Kaynak, A Hacioglu & F Ince (eds), RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies., 7208445, RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies, Institute of Electrical and Electronics Engineers Inc., pp. 777-782, 7th International Conference on Recent Advances in Space Technologies, RAST 2015, Istanbul, Turkey, 16/06/15. https://doi.org/10.1109/RAST.2015.7208445

Unscented Kalman Filter based two-stage estimation of spacecraft position and velocity with single station antenna tracking data. / Hajiyev, Chingiz; Ata, Melih.
RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies. ed. / M. Fevzi Unal; Suleyman Basturk; Okyay Kaynak; Abdurrahman Hacioglu; Fuat Ince. Institute of Electrical and Electronics Engineers Inc., 2015. p. 777-782 7208445 (RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies).

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

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N2 - In this study, a two-stage approach for estimation of spacecraft's position and velocity by single station antenna tracking data is proposed. In the first stage, direct nonlinear antenna measurements are transformed to linear x-y-z coordinate measurements of spacecraft's position, and statistical characteristics of orbit determination errors are analyzed. Variances of orbit parameters' errors are chosen as the accuracy criteria. In the second stage, the outputs of the first stage are improved by the designed Unscented Kalman Filter (UKF) for estimation of the spacecraft's position and velocity on indirect linear x-y-z measurements. In simulations, position and velocity values of a geostationary satellite are found via proposed two-stage procedure.

AB - In this study, a two-stage approach for estimation of spacecraft's position and velocity by single station antenna tracking data is proposed. In the first stage, direct nonlinear antenna measurements are transformed to linear x-y-z coordinate measurements of spacecraft's position, and statistical characteristics of orbit determination errors are analyzed. Variances of orbit parameters' errors are chosen as the accuracy criteria. In the second stage, the outputs of the first stage are improved by the designed Unscented Kalman Filter (UKF) for estimation of the spacecraft's position and velocity on indirect linear x-y-z measurements. In simulations, position and velocity values of a geostationary satellite are found via proposed two-stage procedure.

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Hajiyev C, Ata M. Unscented Kalman Filter based two-stage estimation of spacecraft position and velocity with single station antenna tracking data. In Unal MF, Basturk S, Kaynak O, Hacioglu A, Ince F, editors, RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies. Institute of Electrical and Electronics Engineers Inc. 2015. p. 777-782. 7208445. (RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies). doi: 10.1109/RAST.2015.7208445

Unscented Kalman Filter based two-stage estimation of spacecraft position and velocity with single station antenna tracking data

Abstract

Publication series

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Bibliographical note

Keywords

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