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Arrival Time Correction

 

 

Two commands are available to perform a barycentric correction on the arrival times. In order to speed up the procedure, a precise correction (keeping into account the position of the spacecraft as well) is applied only to the sampling times contained in the orbit data (sample every second). The correction to the arrival times is performed then by interpolating the correction computed for the orbit times.

Thus, in order to apply the barycentric correction to the photon arrival times, it is necessary first to run a command to compute the barycentric correction on the times contained in the orbit file (CORRECT/ORBIT_DATA). This command takes in input the orbit data corresponding to the observation for which the correction is needed, and the equatorial coordinates of the source which has to be corrected (epoch 2000.0), and gives in output a table containing the uncorrected and the corrected orbit times. The output table has four columns, containing respectively the integer part and the fractional part of the original times and of the corrected times. The JPL DE200 ephemeris   [Standish Jr.1982] are used. The syntax of the command and the meaning of the command line parameters is:

CORRECT/ORBIT_DATA output_table alpha delta orbit_table

Then, the data can be corrected with the command CORRECT/BARYCENTER. This command takes in input the table in output from CORRECT/ORBIT_DATA command, and the equatorial coordinates of the source to be corrected (epoch 2000.0), and corrects in place the arrival times, converted to UTC starting from the epoch written into the descriptor CORR_OFFSET. The photon arrival times are then expressed in seconds starting from that epoch. Notice that this descriptor is not propagated by any other EXSAS command: it is thus advisable to apply the barycentric correction only as the last step before running the timing analysis commands. The source coordinates are not used for the computation, but they are requested in order to test the compatibility with the input table (from CORRECT/ORBIT_DATA). The correction is computed by means of a linear interpolation between the corrected orbit times (which have a 1 min sampling time). The syntax of CORRECT/BARYCENTER and the meaning of its parameters is:

CORRECT/BARYCENTER data_table corr_table alpha delta

The correlation between Spacecraft Clock and Universal Time is based on interpolations of calibration points. The coefficients and time boundaries for the polynomials are read in from a MIDAS table located in the calibration area: $exsas_cal:scc_to_utc2.tbl. Each row of the table contains the information about the interpolation for a specific interval of time. The structure of the table is:

   table8572
Table 7.9: Structure of the SCC to UTC calibration table

In the present version, only polynomial functions are used: to get the UTC from a value of SCC the following formula can be used:

displaymath18953


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Next: Folding Search - Period Up: 7.2 The Timing Analysis Previous: Conversion from Spacecraft Clock

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