@inproceedings{fd79bdd63e7c428896c6d5c9294dd4a3,
title = "UKF-based INS/single-satellite Navigation Dynamic Positioning Algorithm",
abstract = "Today's GNSS systems are capable of providing high-precision positioning services. However, GNSS positioning can be rapidly deployed in the absence of constellation navigation systems such as war. This paper proposes a single-satellite positioning method based on inertial navigation system (INS) and Doppler pseudorange difference. The INS component is used to solve the single-satellite positioning results under dynamic conditions. And the positioning results of the target are obtained after positioning iteration and fusion filtering, which can effectively improve the positioning accuracy of single-satellite navigation under dynamic environment. Comparing with Doppler single satellite positioning system based on least squares-Newton iteration and EKF under comprehensive error conditions, the positioning error of this algorithm is only 4\% and 46\% of the above two algorithms. The basic positioning service that can provide dynamic targets in special environment.",
keywords = "INS, least squares, pseudo range difference, single satellite positioning, UKF",
author = "Donghao Liu and Chengkai Tang and Yi Zhang",
note = "Publisher Copyright: {\textcopyright} 2018 IEEE.; 8th IEEE International Conference on Signal Processing, Communications and Computing, ICSPCC 2018 ; Conference date: 14-09-2018 Through 16-09-2018",
year = "2018",
month = dec,
day = "6",
doi = "10.1109/ICSPCC.2018.8567800",
language = "英语",
series = "2018 IEEE International Conference on Signal Processing, Communications and Computing, ICSPCC 2018",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
booktitle = "2018 IEEE International Conference on Signal Processing, Communications and Computing, ICSPCC 2018",
}