<?xml version="1.0" encoding="utf-8" standalone="no"?>
<!DOCTYPE article SYSTEM "http://www.adv-geosci.net/inc/adgeo/copernicus.dtd">
<article language="en">
	<journal>
		<journal_title>Advances in Geosciences</journal_title>
		<journal_url>www.adv-geosci.net</journal_url>
		<issn>1680-7340</issn>
		<eissn>1680-7359</eissn>
		<volume_number>1</volume_number>
		<volume_title>G1. The new gravity field mission (CHAMP, GRACE, GOCE): from measurements to geophysical interpretation</volume_title>
		<publication_year>2003</publication_year>
	</journal>
	<doi>10.5194/adgeo-1-109-2003</doi>
	<article_url>http://www.adv-geosci.net/1/109/2003/</article_url>
	<abstract_html>http://www.adv-geosci.net/1/109/2003/adgeo-1-109-2003.html</abstract_html>
	<fulltext_pdf>http://www.adv-geosci.net/1/109/2003/adgeo-1-109-2003.pdf</fulltext_pdf>
	<start_page>109</start_page>
	<end_page>112</end_page>
	<publication_date>2003-06-30</publication_date>
	<article_title content_type="html">Satellite orbit determination using satellite gravity gradiometry observations in GOCE mission perspective</article_title>
	<authors>
		<author numeration="1" affiliations="1">
			<name>A. Bobojć</name>
		</author>
		<author numeration="2" affiliations="1">
			<name>A. Drożyner</name>
		</author>
	</authors>
	<affiliations>
		<affiliation numeration="1" content_type="html">University of Warmia and Mazury, Institute of Geodesy, ul. Oczapowskiego 1, 10-950 Olsztyn, Poland</affiliation>
	</affiliations>
	<abstract content_type="html">Between the years 2004 and 2005 the launch of
the first gradiometric satellite is planned. This satellite will
be an important element of the Gravity Field and Steady
– State Ocean Circulation Explorer Mission (GOCE). This
mission is one of the reasons for performing the simulation
research of the Satellite Gravity Gradiometry. Our work
contains the theory description and simulation results of the
satellite orbit determination using the gravity tensor observations.
In the process of the satellite orbit determination the
initial dynamic state vector corrections are obtained. These
corrections are estimated by means of the gravity gradiometry
measurements. The performed simulations confirm the
possibility of satellite orbit determination by means of the
gravity tensor observations.&lt;br&gt;&lt;br&gt;&lt;b&gt;Key words.&lt;/b&gt; satellite geodesy, satellite gradiometry, satellite
orbits</abstract>
	<references>
	</references>
</article>

