A 16-parameter GEO Broadcast Ephemeris

Currently, the broadcast ephemerides used in GEOs are same as those of the MEOs and IGSOs in the BeiDou navigation constellation. However, a trade-off strategy, i.e. an orbital inclination of 5° rotation, is needed in the fitting algorithm to solve the ephemeris parameters as well as the user satell...

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Main Author: Zhongkai ZHANG,Lan DU,Li LIU,Feng HE,Yu LU,Peiyuan ZHOU
Format: Article
Language:English
Published: Surveying and Mapping Press 2018-12-01
Series:Journal of Geodesy and Geoinformation Science
Subjects:
Online Access:http://jggs.sinomaps.com/fileup/2096-5990/PDF/1574242792229-1540524397.pdf
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spelling doaj-9a19070b82c341068a8d4f349dcd42f92020-11-25T02:32:39ZengSurveying and Mapping PressJournal of Geodesy and Geoinformation Science2096-59902018-12-01114652A 16-parameter GEO Broadcast EphemerisZhongkai ZHANG,Lan DU,Li LIU,Feng HE,Yu LU,Peiyuan ZHOU01. Zhengzhou Institute of Surveying and Mapping, Zhengzhou 450001, China;2. Beijing Global Information Application and Development Center, Beijing 100094, ChinaCurrently, the broadcast ephemerides used in GEOs are same as those of the MEOs and IGSOs in the BeiDou navigation constellation. However, a trade-off strategy, i.e. an orbital inclination of 5° rotation, is needed in the fitting algorithm to solve the ephemeris parameters as well as the user satellite position computation for GEOs. Based on the standard broadcast ephemerides, the representations of both the orbit and its perturbation were revised according to the second class of nonsingular orbital elements. In this research, a 16-parameter broadcast ephemeris is presented specifically for GEOs,and user satellite position computation formulas were derived correspondingly. Fit simulations show that the root of mean squares (RMS) of user range error (URE) with two hour and three hour data sets are better than 0.05m and 0.1m, respectively.http://jggs.sinomaps.com/fileup/2096-5990/PDF/1574242792229-1540524397.pdf|geo satellites|broadcast ephemeris parameters|nonsingular orbital elements|perturbation|user range error(ure)
collection DOAJ
language English
format Article
sources DOAJ
author Zhongkai ZHANG,Lan DU,Li LIU,Feng HE,Yu LU,Peiyuan ZHOU
spellingShingle Zhongkai ZHANG,Lan DU,Li LIU,Feng HE,Yu LU,Peiyuan ZHOU
A 16-parameter GEO Broadcast Ephemeris
Journal of Geodesy and Geoinformation Science
|geo satellites|broadcast ephemeris parameters|nonsingular orbital elements|perturbation|user range error(ure)
author_facet Zhongkai ZHANG,Lan DU,Li LIU,Feng HE,Yu LU,Peiyuan ZHOU
author_sort Zhongkai ZHANG,Lan DU,Li LIU,Feng HE,Yu LU,Peiyuan ZHOU
title A 16-parameter GEO Broadcast Ephemeris
title_short A 16-parameter GEO Broadcast Ephemeris
title_full A 16-parameter GEO Broadcast Ephemeris
title_fullStr A 16-parameter GEO Broadcast Ephemeris
title_full_unstemmed A 16-parameter GEO Broadcast Ephemeris
title_sort 16-parameter geo broadcast ephemeris
publisher Surveying and Mapping Press
series Journal of Geodesy and Geoinformation Science
issn 2096-5990
publishDate 2018-12-01
description Currently, the broadcast ephemerides used in GEOs are same as those of the MEOs and IGSOs in the BeiDou navigation constellation. However, a trade-off strategy, i.e. an orbital inclination of 5° rotation, is needed in the fitting algorithm to solve the ephemeris parameters as well as the user satellite position computation for GEOs. Based on the standard broadcast ephemerides, the representations of both the orbit and its perturbation were revised according to the second class of nonsingular orbital elements. In this research, a 16-parameter broadcast ephemeris is presented specifically for GEOs,and user satellite position computation formulas were derived correspondingly. Fit simulations show that the root of mean squares (RMS) of user range error (URE) with two hour and three hour data sets are better than 0.05m and 0.1m, respectively.
topic |geo satellites|broadcast ephemeris parameters|nonsingular orbital elements|perturbation|user range error(ure)
url http://jggs.sinomaps.com/fileup/2096-5990/PDF/1574242792229-1540524397.pdf
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