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Real-Time Precise Orbit Determination for LEO between Kinematic and Reduced-Dynamic with Ambiguity Resolution

Wang, Zhiyu and Li, Zishen and Wang, Ningbo and Hoque, Mohammed Mainul and Wang, Liang and Li, Ran and Zhang, Yang and Yuan, Hong (2022) Real-Time Precise Orbit Determination for LEO between Kinematic and Reduced-Dynamic with Ambiguity Resolution. Aerospace. Multidisciplinary Digital Publishing Institute (MDPI). doi: 10.3390/aerospace9010025. ISSN 2226-4310.

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Official URL: https://www.mdpi.com/2226-4310/9/1/25

Abstract

The real-time integer-ambiguity resolution of the carrier-phase observation is one of the most effective approaches to enhance the accuracy of real-time precise point positioning (PPP), kinematic precise orbit determination (KPOD), and reduced-dynamic precise orbit determination (RPOD) for low earth orbit (LEO) satellites. In this study, the integer phase clock (IPC) and wide-lane satellite bias (WSB) products from CNES (Centre National d’Etudes Spatiales) are used to fix ambiguity in real time. Meanwhile, the three models of real-time PPP, KPOD, and RPOD are applied to validate the contribution of ambiguity resolution. Experimental results show that (1) the average positioning accuracy of IGS stations for ambiguity-fixed solutions is improved from about 7.14 to 5.91 cm, with an improvement of around 17% compared to the real-time float PPP solutions, with enhancement in the east-west direction particularly significant, with an improvement of about 29%; (2) the average accuracy of the estimated LEO orbit with ambiguity-fixed solutions in the real-time KPOD and RPOD mode is improved by about 16% and 10%, respectively, with respect to the corresponding mode with the ambiguity-float solutions; (3) the performance of real-time LEO RPOD is better than that of the corresponding KPOD, regardless of fixed- or float-ambiguity solutions. Moreover, the average ambiguity-fixed ratio can reach more than 90% in real-time PPP, KPOD, and RPOD

Item URL in elib:https://elib.dlr.de/189042/
Document Type:Article
Title:Real-Time Precise Orbit Determination for LEO between Kinematic and Reduced-Dynamic with Ambiguity Resolution
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Wang, ZhiyuUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Li, ZishenUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Wang, NingboUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Hoque, Mohammed MainulUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Wang, LiangUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Li, RanUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Zhang, YangCASUNSPECIFIEDUNSPECIFIED
Yuan, HongUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2022
Journal or Publication Title:Aerospace
Refereed publication:Yes
Open Access:Yes
Gold Open Access:Yes
In SCOPUS:Yes
In ISI Web of Science:Yes
DOI:10.3390/aerospace9010025
Publisher:Multidisciplinary Digital Publishing Institute (MDPI)
ISSN:2226-4310
Status:Published
Keywords:real-time; ambiguity resolution; low earth orbit; precise point positioning; kinematic precise orbit determination; reduced-dynamic precise orbit determination
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Earth Observation
DLR - Research area:Raumfahrt
DLR - Program:R EO - Earth Observation
DLR - Research theme (Project):R - Solar-Terrestrial Physics SO
Location: Neustrelitz
Institutes and Institutions:Institute for Solar-Terrestrial Physics > Space Weather Observation
Deposited By: Hoque, Mohammed Mainul
Deposited On:31 Oct 2022 18:28
Last Modified:31 Oct 2022 18:28

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