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IS-GPS-800A - US Coast Guard Navigation Center

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3.5.4.2.3 User Algorithm for Application of the EOPThe EOP fields in subframe 3, page 2 contain the EOP needed to construct the ECEF-to-ECI coordinatetransformation. The user computes the ECEF position of the SV antenna phase center using the equations shown inTable 3.5-2. The coordinate transformation, for translating to the corresponding ECI SV antenna phase centerposition, is derived using the equations shown in Section 30.3.3.5.1.1 and Table 30-VIII of <strong>IS</strong>-<strong>GPS</strong>-200. Thecoordinate systems are defined in Section 20.3.3.4.3.3 of <strong>IS</strong>-<strong>GPS</strong>-200.Table 3.5-5.Earth Orientation ParametersParameterNo. ofBits**ScaleFactor(LSB)EffectiveRange***Unitst EOPPM_X †PM_XPM_Y ††PM_YUT1 †††UT1 †††EOP Data Reference TimeX-Axis Polar Motion Valueat Reference Time.X-Axis Polar Motion Drift atReference Time.Y-Axis Polar Motion Valueat Reference Time.Y-Axis Polar Motion Drift atReference Time.UT1-UTC Difference atReference Time.Rate of UT1-UTCDifference at ReferenceTime1621*15*21*15*31*19*2 42 -202 -212 -202 -212 -242 -25 604,78417.8125 x 10 -317.8125 x 10 -3647.8125 x 10 -3 secondsarc-secondsarc-seconds/dayarc-secondsarc-seconds/daysecondsseconds/day* Parameters so indicated are in two’s complement notation;** See Figure 3.5-3 for complete bit allocation in subframe 3, page 2;*** Unless otherwise indicated in this column, effective range is the maximum range attainable withindicated bit allocation and scale factor.†Represents the predicted angular displacement of instantaneous Celestial Ephemeris Pole with respect tosemi-minor axis of the reference ellipsoid along Greenwich meridian.††Represents the predicted angular displacement of instantaneous Celestial Ephemeris Pole with respect tosemi-minor axis of the reference ellipsoid on a line directed 90 west of Greenwich meridian.†††With zonal tides restored.56 <strong>IS</strong>-<strong>GPS</strong>-<strong>800A</strong>8 June 2010

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