Earth's pole coordinates determined from Lageos-1/2 laser ranging

The Earth's pole coordinates, obtained from satellite laser ranging data of Lageos-1 and Lageos-2 are presented. The procedure, used models and algorithms are described. Results are compared with similar series from IERS database.

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Veröffentlicht in:Advances in Astronomy and Space Physics
Datum:2014
Hauptverfasser: Zhaborovskyy, V.P., Choliy, V.Ya.
Format: Artikel
Sprache:English
Veröffentlicht: Головна астрономічна обсерваторія НАН України 2014
Online Zugang:https://nasplib.isofts.kiev.ua/handle/123456789/119816
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Zitieren:Earth's pole coordinates determined from Lageos-1/2 laser ranging / V.P. Zhaborovskyy, V.Ya. Choliy // Advances in Astronomy and Space Physics. — 2014. — Т. 4., вип. 1-2. — С. 54-57. — Бібліогр.: 8 назв. — англ.

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Digital Library of Periodicals of National Academy of Sciences of Ukraine
id nasplib_isofts_kiev_ua-123456789-119816
record_format dspace
spelling Zhaborovskyy, V.P.
Choliy, V.Ya.
2017-06-09T20:19:06Z
2017-06-09T20:19:06Z
2014
Earth's pole coordinates determined from Lageos-1/2 laser ranging / V.P. Zhaborovskyy, V.Ya. Choliy // Advances in Astronomy and Space Physics. — 2014. — Т. 4., вип. 1-2. — С. 54-57. — Бібліогр.: 8 назв. — англ.
2227-1481
DOI: 10.17721/2227-1481.4.54-57
https://nasplib.isofts.kiev.ua/handle/123456789/119816
The Earth's pole coordinates, obtained from satellite laser ranging data of Lageos-1 and Lageos-2 are presented. The procedure, used models and algorithms are described. Results are compared with similar series from IERS database.
en
Головна астрономічна обсерваторія НАН України
Advances in Astronomy and Space Physics
Earth's pole coordinates determined from Lageos-1/2 laser ranging
Article
published earlier
institution Digital Library of Periodicals of National Academy of Sciences of Ukraine
collection DSpace DC
title Earth's pole coordinates determined from Lageos-1/2 laser ranging
spellingShingle Earth's pole coordinates determined from Lageos-1/2 laser ranging
Zhaborovskyy, V.P.
Choliy, V.Ya.
title_short Earth's pole coordinates determined from Lageos-1/2 laser ranging
title_full Earth's pole coordinates determined from Lageos-1/2 laser ranging
title_fullStr Earth's pole coordinates determined from Lageos-1/2 laser ranging
title_full_unstemmed Earth's pole coordinates determined from Lageos-1/2 laser ranging
title_sort earth's pole coordinates determined from lageos-1/2 laser ranging
author Zhaborovskyy, V.P.
Choliy, V.Ya.
author_facet Zhaborovskyy, V.P.
Choliy, V.Ya.
publishDate 2014
language English
container_title Advances in Astronomy and Space Physics
publisher Головна астрономічна обсерваторія НАН України
format Article
description The Earth's pole coordinates, obtained from satellite laser ranging data of Lageos-1 and Lageos-2 are presented. The procedure, used models and algorithms are described. Results are compared with similar series from IERS database.
issn 2227-1481
url https://nasplib.isofts.kiev.ua/handle/123456789/119816
citation_txt Earth's pole coordinates determined from Lageos-1/2 laser ranging / V.P. Zhaborovskyy, V.Ya. Choliy // Advances in Astronomy and Space Physics. — 2014. — Т. 4., вип. 1-2. — С. 54-57. — Бібліогр.: 8 назв. — англ.
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first_indexed 2025-11-24T04:21:13Z
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fulltext Earth's pole coordinates determined from Lageos-1/2 laser ranging V.P. Zhaborovskyy1∗, V.Ya.Choliy1,2 Advances in Astronomy and Space Physics, 4, 54-57 (2014) © V.P. Zhaborovskyy, V.Ya.Choliy, 2014 1Main Astronomical Observatory of NAS of Ukraine, Akademika Zabolotnoho str., 27, 03680 Kyiv, Ukraine 2Taras Shevchenko National University of Kyiv, Glushkova ave., 4, 03127, Kyiv, Ukraine The Earth's pole coordinates, obtained from satellite laser ranging data of Lageos-1 and Lageos-2 are presented. The procedure, used models and algorithms are described. Results are compared with similar series from IERS database. Key words: methods: data analysis, reference system, geodesy introduction During the past 40 years the precision of Satellite Laser Ranging (SLR) has changed dramatically. To- gether with greater computational capabilities and better algorithms for data storage, searching, and analysis, the overall precision of the geodynam- ics and geodetic tasks was substantially improved. Among the methods substantially improved, the de- termination of the Earth' pole motion and irregu- larities of Earth' spin velocity are the central ones. The Lageos-1 (1976) and Lageos-2 (1992) satellites were launched speci�cally to accomplish these tasks. These satellites are modelled as mathematical point- mass. They are spherically shaped, and their orbits were designed to diminish the in�uence of di�erent poorly-modelled accelerations, as to allow relatively e�ortless laser ranging. The processing of the ob- servations allows the International Earth Rotation Service to create and distribute o�cial time correc- tions and pole coordinate series for users worldwide. Such a result is not possible without extensive inter- national collaboration and independent data analy- sis centres capable of creating independent solutions. These are the essential components of the work co- ordinated by IERS. Since 1987, a data analysis centre of satellite laser ranging (SLR) has been in operation on a per- manent basis at the Main Astronomical Observa- tory of NAS . The previously used software pack- age KyivGeodynamics is outdated, as over the past ten years the IERS introduced signi�cant changes to their Standards [5] three times. That is why the new version of the code was created [8], called KyivGeodynamics++ (hereinafter KG++). To validate the new code the processing of the SLR data for 2001 was conducted. the procedure of calculation The algorithm of data processing is based upon the linearised Least Squares method. The observed distance between the satellite and the station ~ρ can be written as: ~ρ(t) = M̂(t)~r(t)− ~R(t) = ~Φ( ~X, t), (1) where ~r(t) is satellite position in International Celes- tial Reference Frame (ICRF), ~R is the station posi- tion in the International Terrestrial Reference Frame (ITRF), andM is the transformation matrix between ITRF and ICRF. Another vector ~Φ( ~X, t) is the vec- tor function (in general case it is highly complicated with regards to the calculation) of the parameters ~X. Observation instruments (telescope, equipped with laser transmitter and receiver) allow us to ob- serve the absolute value of, say ~ρ, the distance to the satellite. Having approximate values for ~X0 the (1) can be linearised, and then ρo − ρc = ( ∂~Φ( ~X) ∂ ~X )∣∣∣∣∣ ~X0 ~x, where ~x = ~X− ~X0 are corrections to the parameters. A su�cient number of observations will give us the possibility to determine a better estimation for ~X. The observational data is processed using a two- stage procedure. During the �rst stage the Kepler ∗zhskyy@gmail.com 54 Advances in Astronomy and Space Physics V. P. Zhaborovskyy, V.Ya.Choliy orbital elements of the satellite are estimated. This step is repeated until the standard deviation of the di�erence observed minus calculated stops decreas- ing. During the second stage, the determined orbit is used to estimate the pole coordinates along with empirical acceleration of the satellite. The latter ac- celeration is widely used to compensate any forgotten accelerations of di�erent origin not explicitly intro- duced in the satellite equation of motion. The elementary processing unit is the arc. It com- prises the observation of a single satellite on a 7-day interval (standard IERS value) together with a full set of vector ~X components derived from it. All of the observations of Lageos-1 and Lageos-2 satellites for the year 2001 were processed for this ar- ticle. There were approximately 75000 normal points in our database. There were 52 seven-day-long arcs: a end point of an arc served as the starting point for the next one. Each arc was processed in two stages. During the �rst stage only Keplerian orbital elements were esti- mated until the overall standard deviation of the ob- served minus calculated values stopped decreasing. This stage lasted 4�5 iterations. Following this, the estimation of the empirical acceleration (one value per day) and pole coordinates (two values per day) took place. Iterations continued until standard the deviation decreased to below 10 cm. The speci�ed 10 cm value is su�cient to estimate pole coordinates. In general, the overall process took 12�15 iterations per arc. The observed minus calculated residuals were thoroughly analysed during the iterations, and their distribution was checked for normality. Rejec- tion criteria was set to 3σ. Sometimes up to 30% of the observations were dropped. New code strictly follows all recommendations from IERS Conventions 2010 [5]. All software mod- ules were written from scratch and tested separately on arti�cial examples before being introduced into productive code. Processing of the Lageos-1 and Lageos-2 data is the �rst result from the release ver- sion code. A brief outline of the models used is presented below. If not speci�ed, the models from IERS Con- ventions were used. forces: � Earth's gravity �eld and ocean tide model EGM96 [6], 20× 20 solution; � Third body gravity: Moon, Sun and all planets � DE421 [4]; � Direct solar radiation pressure: re�ectance co- e�cient a priori 1.14; � Indirect light pressure: using cylindrical shadow function; � Relativistic correction. reference frame: � Stations coordinates and stations velocities: ITRF2005 solution, epoch 2000.0 [1]; � Precession and nutation: full IAU2000A model [2]; � Polar motion: C04 IERS; � Tidal e�ects. other: � Observations: all normal points for 2001 year from CDDIS database for Lageos-1 and Lageos- 2; � Tropospheric refraction: Marini/Murray model [7]; � Constants (speed of light, gravitational con- stant etc.) from IERS Conventions. estimated parameters: � Estimation criteria: 3σ ' 5 cm for �nal result; � O-C �lter: 3σ for each iteration; � Satellite orbital elements are determined as one set per 7 days arc; � Pole coordinates determined for each day; � Empirical acceleration coe�cient determined for each day. results The X and Y pole coordinates were determined for every day of 2001 from the observations of a sin- gle satellite. The results are presented in Fig. 1 and Fig. 2 for Lageos-1 and Lageos-2. The standard de- viation for the last iteration of each one-day arc does not exceed 10 cm for Lageos-1 and 7 cm for Lageos-2. This result was compared with analogous data obtained in di�erent international data analysis cen- tres. All of these data are available online1. We used the series by the Center for Space Research, USA (crs), Delft University of Technology, Nether- land (dut), Institute for Applied Astronomy, Russia (iaa) and standard ILRS solutions (ilrs) (see Fig. 3). The method of comparison is based upon Helmert transform and described in [3]. On the �rst stage, having two di�erent sets of polar data, one can ex- tract systematic di�erences of these sets by applying a 6-parameter Helmert transform: 1ftp://hpiers.obspm.fr/iers/series/operational 55 Advances in Astronomy and Space Physics V. P. Zhaborovskyy, V.Ya.Choliy −0.2 −0.1 0.0 0.1 0.2 0.3 X pole, marcsec 0.1 0.2 0.3 0.4 0.5 Y p o le , m ar cs ec 01.01.2001 31.12.2001 Earth X and Y pole by Lageos 1 observations. Fig. 1: Earth pole from Lageos-1 observation. −0.2 −0.1 0.0 0.1 0.2 0.3 X pole, marcsec 0.1 0.2 0.3 0.4 0.5 Y p o le , m ar cs ec 01.01.2001 31.12.2001 Earth X and Y pole by Lageos 2 observations. Fig. 2: Earth pole from Lageos-2 observation. −0.2 −0.1 0.0 0.1 0.2 0.3 X pole, marcsec 0.10 0.15 0.20 0.25 0.30 0.35 0.40 0.45 0.50 Y p o le , m ar cs ec 01.01.2001 31.12.2001 Earth X and Y pole by ILRS Fig. 3: Earth pole from ILRS. −0.2 −0.1 0.0 0.1 0.2 0.3 X pole, marcsec 0.10 0.15 0.20 0.25 0.30 0.35 0.40 0.45 0.50 Y p o le , m ar cs ec 01.01.2001 31.12.2001 01.01.2001 31.12.2001 01.01.2001 31.12.2001 Earth X and Y pole by Lageos 1/2 observations. Fig. 4: Earth pole � all results. ~r2 − ~r1 = [ a11 a12 a21 a22 ] ~r1 + [ b1 b2 ] , where ~r is the vector containing two pole coordinates, where systematics error are described as rotations (aij , i 6= j) scales (aii) and shifts (bk). Following this, mutual standard deviations σij of series are ob- tained: σ2 ij = N∑ k=1 ( ~r(i)k − ~r∗(j)k )2 N −M , where M is the number of degrees of freedom, and the symbol ∗ is used to signal the series without sys- tematic errors. The own standard deviations of the series may be obtained if a su�cient number of σij is obtained from the equation: σ2 12 = σ2 1 + σ2 2 − 2ρ12σ1σ2, σ2 13 = σ2 1 + σ2 3 − 2ρ13σ1σ3, σ2 23 = σ2 2 + σ2 3 − 2ρ23σ2σ3, where ρij are the correlations of the corresponding series. Varying solutions were used as a base for compar- ison. Three series were compared. The computed standard deviations are given in Table 1 where every cell contains the resulting value found by compar- ing our satellite solution (row name) and two cen- tre names given as the column headings. The mean standard deviation of pole coordinates obtained from Lageos-1 observations is 3.10 × 10−4, and that ob- tained from Lageos-2 observations is 1.19× 10−3. All series of pole coordinates are present in Fig. 4. 56 Advances in Astronomy and Space Physics V. P. Zhaborovskyy, V.Ya.Choliy Table 1: Standard deviations in mas of some Earth pole coordinates series. dut � csr csr � iaa iaa � ilrs ilrs � dut mean Lag1 2.98 · 10−4 3.57 · 10−4 2.44 · 10−4 3.42 · 10−4 3.10 · 10−4 Lag2 1.27 · 10−3 1.22 · 10−3 1.21 · 10−3 1.04 · 10−3 1.19 · 10−3 conclusions The values presented in Table 1 show two main points. Firstly, the precision of Lageos-1 based pole coordinates are nearly one order of magnitude better than the values from processing Lageos-2 data. The second point is that in any case both of the preci- sions agree with values produced by other data anal- ysis centres. This result demonstrates the correct work of KG++ on 2 cm precision level and its applica- bility for the analysis of the SLR data with precision su�cient for IERS tasks. references [1] Altamimi Z., Collilieux X., Legrand J., Garayt B. & BoucherC. 2007, J. Geophys. Res., 112, B09401 [2] Capitaine N., Chapront J., Lambert S. & Wallace P. T. 2003, A&A, 400, 1145 [3] CholiyV.Ya. 2014, Advances in Astronomy and Space Physics, 4, 15 [4] FolknerW.M., Williams J.G. & BoggsD.H. 2009, The In- terplanetary Network Progress Report, 178, 1 [5] IERS Technical Note No. 36 (IERS Conventions 2010), 2010, IERS Conventions Center [6] LemoineF., Kenyon S., Factor J. et al. 1998, `The De- velopment of the Joint NASA GSFC and National Im- agery and Mapping Agency (NIMA) Geopotential Model EGM96', NASA/TP-1998-206861, Goddard Space Flight Center, Greenbelt [7] Marini J. & MurrayC. 1973, `Correction of laser range tracking data for atmospheric refraction at elevations above 10 degrees', NASA-TM-X-70555, GSFC, Greenbelt [8] CholiyV.Ya. & ZhaborovskyyV.P. 2011, Advances in As- tronomy and Space Physics, 1, 96 57 Advances in Astronomy and Space Physics 58