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29 3 Vol.29, No. 3 2011 7 PROGRESS IN ASTRONOMY Jul., 2011 1000-8349(2011)03-343-10 AR ( 410083 ) AR 3 X Y AR P183.3 A 1 (Polar Motion, PM) [1] X Y (LOD) (ERP) [2] ERP ( VLBI SLR GPS ) ERP ERP [3–5] ERP ERP [6] ERP [4–15] Zhu [9, 10] (AW) (CW) ( 2011-03-08 2011-05-24 (10878026) (2011ssxt054)

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    �°ÝJpk½^§4£ýÿ�«ë{¶�T{4£ýÿ�«#�}

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    ¥¥¥ããã©©©aaaÒÒÒµµµP183.3 ©©©zzzIII£££èèèµµµA

    1 Ú ó

    4£ (Polar Motion, PM)́ L�/¥g=$Ä�ëꧧ´/¥]g=¶

    3/¥�NS$Ä�4:3/¥L¡þ� u)úCz�y[1]"4£3/4

    IX¥§q© X ©þÚ Y ©þ§§ÚFCz (LOD)Ú¡/¥g=ëê (ERP)[2]"p°

    ÝERP�¼�´/¥ëµeÚU¥ëµem?1p=�7^§Ïd§éu¥

    (�Ê!�&ÿ�A^ÚïÄäk¿Â"yÿ/Eâ ($ÄZ�ÿþ§VLBI¶¥

    (-1ÿå§SLR¶�¥½ XÚ§GPS¶��)´8c¼�ERP�ÌÃã§,duE,�

    êâ?nL§§ERP�(J¿ØU¢/¼�[3–5]"Ïd§éERP�áÏýÿÒw�c7§

    éERP�¥Ïýÿäk©�nØdÚ¢S¿Â[6]"ERP�|¤Ü©§

    4£ýÿÒäk©�¿Â"

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    [9, 10]ѵ

    â4£¥±c (AW) Úa�V (CW)äk½�(½5 (±cÚa�V��Ì!

    ÂvFϵ2011-03-08¶ ?£Fϵ2011-05-24

    ]Ï8µI[g,ÆÄ7¬¥IÆ�U©éÜÄ7(10878026)¶¥HÆïÄ)Æ Ø©M#Ä7(2011ssxt054)

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    ��¦{[ܦ)�.ëê§l¢y4£íýÿ�8�"��NõÆöUJÑ«

    |Ü�.�{é4£?1ýÿ[4–8, 12, 13]

    §XSchuh[4]JÑ��¦{Ú

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    ü  a¶X(t) t�4£X©þ�[10]"Ó�éu4£ Y S��.§éAëêL

    «¹Â XS��.�"

    \���¦{�.��¦{�.�«O´3¦)ëê\�Ý P§äN

    ¦){Xe§�:

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    Ax Bx C1x C2x D

    1x D

    2x E

    1x E

    2x

    Ay By C1y C2y D

    1y D

    2y E

    1y E

    2y

    , (3)

    B =

    1 t1 cos (2πt1PSA

    ) sin (2πt1PSA

    ) cos (2πt1PA

    ) sin (2πt1PA

    ) cos (2πt1PC

    ) sin (2πt1PC

    )

    1 t2 cos (2πt2PSA

    ) sin (2πt2PSA

    ) cos (2πt2PA

    ) sin (2πt2PA

    ) cos (2πt2PC

    ) sin (2πt2PC

    )

    .

    .

    ....

    .

    .

    ....

    .

    .

    ....

    .

    .

    ....

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    ) sin (2πtnPSA

    ) cos (2πtnPA

    ) sin (2πtnPA

    ) cos (2πtnPC

    ) sin (2πtnPC

    )

    , (4)

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    X̂(t1) X̂(t2) · · · X̂(tn)

    Ŷ(t1) Ŷ(t2) · · · Ŷ(tn)

    , (5)

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    2.2 �Ý�À�

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    f =PtiPt j

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    Pi =1

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    j=1

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    t=M+1

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    j=1

    ϕ jzt− j)2. (13)

    3¢Sýÿ¥§PM ´^ AR(M) �.[Ü zt (t = 1, 2, 3, · · · , n) S��{þ�"�

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    n∑

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    ´4£�Ì-u§4£«ºÝ�Cz�Éù-uÏ�K[20, 21]¶�©3é4

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    ë©zµ

    [1] �,HS²,4m�./ÿþÆÄ:.ÉÇ:ÉÇÆÑ�. 2008µ17

    [2] Òu,ë.U©/¥ÄåÆ.LH:ìÀÆEâÑ�.2000, 26: 466

    [3] 7©¹.U©Æ?Ð, 2007, 25(4): 346

    [4] Schuh H, Ulrich M, Egger D, et al. J. Geod, 2002, 76: 247

    [5] Akyilmaz O, Kutterer H J. Geod, 2004, 78: 82

    [6] �j'.Ƭة.þ°:¥IÆ�þ°U©�, 2007: 1

    [7] NÈ,±[÷.1ìÿÆ�, 2010, 29(2): 70

    [8] �j',�S,±[÷.ÆÏ�, 2007, 52(15): 1728

    [9] Zhu S Y. Prediction of Earth Rotation and Polar Motion. http://adsabs.harvard.edu/abs/1981perp.rept.....Z, 1981: 2

    [10] Zhu S Y. Bull Geod, 1982, 56: 258

    [11] Chao B F. Bull Geod, 1985, 59: 81

    [12] Kosek W, McCarthy D D, Johnson T J, et al. Astrometry, geodynamics and Solar system dynamics: from milliarcseconds to microarc-

    seconds. St. Petersburg: Inst. of Applied Astronomy of the Russian Acad. of Sciences, 2004: 164

    [13] Kosek W, Kalarus M, Niedzielski T. The Celestial Reference Frame for the Future. Paris: Observatoire de Paris SystYmes de RWfWrence

    Temps-Espace UMR8630/CNRS, 2008: 155

    [14] Iz H B. J. Geod, 2008, 82: 871

    [15] Kalarus M, Schch H, Kozek W, et al. J. Geod, 2010, 84: 587

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    [17] Schuh H, Nagel S, Seitz T. J. Geod, 2001, 74: 701

    [18] 4#,>�>,Áï�,�.¢^ÿþêâ?n{.�®:ÿ±Ñ�, 2000: 83

    [19] ¶�I.U©êâ?n{.H®:H®ÆÑ�, 1998: 307

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  • 352 U © Æ ? Ð 29ò352 U © Æ ? Ð 29ò352 U © Æ ? Ð 29ò

    Joint Model of Weighted Least-squares and AR in Prediction of Polar

    Motion

    ZHANG Hao, WANG Qi-jie, ZHU Jian-jun, ZHANG Xiao-hong

    (School of Geosciences and Info-Physics, Central South University, Changsha 4100833, China)

    Abstract: Earth rotation parameters (ERPs) include length of day and polar motion. Precise trans-

    formations between the international celestial and terrestrial reference frames are needed for many

    advanced geodetic and astronomical tasks including positioning and navigation on Earth and in

    space. To perform this transformation, accurate ERPs are necessary. However, the precise measure-

    ments of ERPs by space-geodetic techniques have to be pre-processed before the ERPs are available.

    This causes a delay of 15 to 20 hours in case of GPS and of a few days in case of very-long-baseline

    interferometry (VLBI) and satellite laser ranging (SLR).Thus it’s necessary to predict the ERPs over

    at least a few days. In addition, it might be interesting to look further into the future to estimate the

    Earth’s rotation in the next few months. Therefore, this paper deals with short-term predictions for

    next 30 days, long-term predictions for 360 days.

    Various prediction methods have been developed, such as thejoint model of least-squares and

    AR, joint model of least-squares and artificial neural networks(ANN), and so on. These methods

    most treat the Chandler Wobble(CW) and Annual Wobble(AW) ofthe polar motion as constants.

    However, the CW and AW are of time variant characteristics asa matter of fact. This paper puts

    forward a new joint model of weighted least-squares(WLS) and AR, according to the time variant

    characteristics of CW and AW. One important issue in building the WLS+AR model is the right

    choice of the weight matrix P. According to the statistical properties of the polar motion series,

    the rule of weight choice is determined: the fitting value nearer to prediction value is given larger

    weight. In accordance with the rule, three kinds of weight function are built and compared in order

    to assess the weight function of the weighted least-squares. The more appropriate weight function

    for X series and Y series are suggested respectively. Finally the WLS+AR model is compared with

    LS+AR model and shown that the new models are effective for improving the accuracy of the PM

    prediction. The model is an interesting and new attempt in the PM prediction, and could be seen

    as an alternative prediction method. However, in the paper,the theoretical basis of the model is not

    analyzed in depth, and which will be further studied in the later research.

    Key words: Polar Motion Prediction; Weighted Least-squares; AR Model; Weight Function