Proceedings of the 3rd International Conference on Mechatronics, Robotics and Automation

Integration of Radar Measurements with Navigation Data for Initial Orbit Estimation

Authors
Nanke Du, Linyang Guo, Junshan Mu, Xuwei Su
Corresponding Author
Nanke Du
Available Online April 2015.
DOI
10.2991/icmra-15.2015.137How to use a DOI?
Keywords
Data fusion finite difference Radar measurements orbit determination precision
Abstract

An introduction is given about the current initial orbit determination mode for tracking ships. The paper proposes a method to improve the current orbit estimation mode by integrating the radar tracking measurements and onboard navigation data. The measurement and system model for the method is given, and related state transition matrix formulation is analyzed. The method is based on Markov and random process theory. The numerical results show that the finite difference method can be a good alternative for the traditional orbit estimation method.

Copyright
© 2015, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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Volume Title
Proceedings of the 3rd International Conference on Mechatronics, Robotics and Automation
Series
Advances in Computer Science Research
Publication Date
April 2015
ISBN
978-94-62520-76-9
ISSN
2352-538X
DOI
10.2991/icmra-15.2015.137How to use a DOI?
Copyright
© 2015, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

Cite this article

TY  - CONF
AU  - Nanke Du
AU  - Linyang Guo
AU  - Junshan Mu
AU  - Xuwei Su
PY  - 2015/04
DA  - 2015/04
TI  - Integration of Radar Measurements with Navigation Data for Initial Orbit Estimation
BT  - Proceedings of the 3rd International Conference on Mechatronics, Robotics and Automation
PB  - Atlantis Press
SP  - 712
EP  - 717
SN  - 2352-538X
UR  - https://doi.org/10.2991/icmra-15.2015.137
DO  - 10.2991/icmra-15.2015.137
ID  - Du2015/04
ER  -