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The ephemeris parameters describe the orbit during a given interval of time (at least one hour) The ephemeris parameters are the parameters for an extension of the orbital model predicted by Kepler The extension is necessary to account for non-uniformities in the Earth gravitational eld The ephemeris parameters are determined by the control segment as a curve t to the measured satellite orbit The parameter toe is the reference time of applicability (local origin) of the ephemeris parameters The ephemeris parameters are de ned in Table C1 [6] These parameters are broadcast by the satellites and available after decoding on-board the receiver The units of the broadcast parameters are also de ned in the table The ECEF coordinates for the phase center of the satellite antenna can be calculated using a variation of the equations shown in Table C2 [131] The main inputs to these equations are the variable tsv and the satellite clock correction and ephemeris parameters de ned in Table C1 The satellite antenna phase center position is very sensitive to small perturbations in most ephemeris parameters The sensitivity of position to the parameters A, Crc , and Crs is about one meter/meter The sensitivity to angular parameters is on the order of 108 meters/semi-circle, and to the angular rate parameters is on the order of 1012 meters/semi-circle/second Because of this extreme sensitivity to angular perturbations, the values of all constants should exactly match those stated in Appendix A, from [6] The parameter IODE is an integer which allows the user to detect when a new set of ephemeris parameters is available By monitoring the IODE value for the incoming satellite signal relative to the IODE of the ephemeris data currently in use, the user can determine when to update the ephemeris model parameters A few comments are appropriate concerning Table C2 The variable tk is the actual total time di erence between the time t and the ephemeris reference time toe The calculation must account for beginning or end of week crossovers That is, if tk is greater than 302,400 seconds, subtract 604,800 seconds from tk If tk is less than -302,400 seconds, add 604,800.

Oracle Exadata Database Machine X2-2

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Parameter TGD IODC toc af 2 af 1 af 0 M0 n e A1/2 0 i0 IDOT Cuc Cus Crc Crs Cic Cis toe IODE

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Description Group Delay, sec Issue of Data, Clock Clock data reference time, sec sec Second order correction to satellite clock, sec2 sec First order correction to satellite clock, sec Constant correction to satellite clock, sec Mean anomaly at reference time, semi-circles Mean motion di erence from computed value, semi-circles/sec Eccentricity, dimensionless Square root of the semi-major axis, m Longitude of ascension node at reference time, semi-circle Inclination angle at reference time, semi-circle Argument of perigee, semi-circle Rate of right ascension, semi-circle/sec Rate of inclination angle, semi-circle/sec Amplitude of the cosine harmonic correction to the argument of latitude, rad Amplitude of the sine harmonic correction to the argument of latitude, rad Amplitude of the cosine harmonic correction to the orbit radius, m Amplitude of the sine harmonic correction to the orbit radius, m Amplitude of the cosine harmonic correction to the angle of inclination, rad Amplitude of the sine harmonic correction to the angle of inclination, rad Ephemeris reference time, sec Issue of Data, Ephemeris

Date of Introduction Server Nodes Storage Cells Total Server Node CPUs and Cores Total Memory Total Flash InfiniBand Switches High Performance Disk Capacity High Capacity Disk Capacity TABLE 4-3

seconds to tk The equation for Ek must be solved iteratively Various iterative solution techniques are considered in [131] Table C3 [44] contains a complete example set of ephemeris parameters By using these ephemeris parameters in the equations of Table C2 the space vehicle (satellite) time o set and ECEF satellite antenna coordinates can be determined The results of these calculations are shown in Table C4

Not shown in the previous tables is the Ethernet switch provided in each Rack for administration of the Database Machine A keyboard, video display unit, and mouse (KVM) are provided for local administration with X2-2 configurations Also included is a spares kit that includes an extra disk and extra Smart Flash Cache card for the Quarter and Half Rack or two extra disks and two extra Smart Flash Cache cards for the Full Rack, and InfiniBand cables Oracle has tightly defined what optimal ratios of components (such as processor cores, memory, and throughput) in database server nodes and storage cells should be Though it is possible to activate only part of a Rack configuration, in Oracle Exadata Database Machines, Oracle recommends that you maintain the ratio of four database server nodes for every seven storage cells in X2-2 configurations if you do That is similar to the ratio that exists in the Half and Full Racks in X2-2 configurations For X2-2 Rack configurations where you activate just a quarter of a Full Rack, use the ratio of two database server nodes and three storage cells The only deviation to

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