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Bernese GPS Software Version 5.0 - Bernese GNSS Software

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5. Preparation of Earth Orientation, <strong>GNSS</strong> Orbit, and Satellite Clock Information<br />

a list of <strong>GPS</strong> RINEX navigation files or a list of GLONASS RINEX navigation files. A<br />

third possibility is to merge GLONASS and <strong>GPS</strong> RINEX navigation message files before<br />

conversion. In this case it is recommended to process one pair of files in one program run.<br />

Each input file (or pair of input files) will be converted into one output precise file.<br />

In the resulting SP3 file the Earth-fixed positions of each satellite and its clock values<br />

are stored in time intervals specified by the user. Normally a time interval of 15 minutes<br />

is appropriate. The program checks the broadcast information for plausibility using the<br />

criteria explained in Section 5.3.3.<br />

The program RXNPRE allows to exclude GLONASS satellites showing a shift in the navigation<br />

messages (e.g., due to a maneuver) from being written to the output precise orbit<br />

file. Shifted <strong>GPS</strong> satellites are skipped in any case (see Section 5.3.3).<br />

In order to process <strong>GPS</strong> and GLONASS data simultaneously, the orbit and clock information<br />

needs to refer to the same reference system and to the same time scale. The GLONASS<br />

broadcast ephemerides are therefore transformed to ITRF and <strong>GPS</strong> system time. For the<br />

transition from PZ–90 (GLONASS reference system) to WGS–84 (<strong>GPS</strong> reference system<br />

which is consistent with the parameters of the ITRS), a rotation of −334.5 mas around<br />

the Z–axis is currently applied to the positions of the GLONASS satellites, see [Habrich,<br />

1999] and [Ineichen et al., 2000]. The transformation values for the transition from PZ–90<br />

to WGS–84 (resp. ITRF) have to be specified in file ${X}/GEN/DATUM.<br />

After having transformed the broadcast RINEX files into SP3 format a standard orbit file in<br />

<strong>Bernese</strong> format may be created using programs PRETAB (”Menu>Orbits/EOP>Create tabular orbits”)<br />

and ORBGEN (”Menu>Orbits/EOP>Create standard orbits”). The procedure is the same as described<br />

in Section 5.4).<br />

For more information about the computation of GLONASS satellite positions using broadcast<br />

ephemerides we refer to [Habrich, 1999].<br />

5.3.2 Alternative Procedure for <strong>GPS</strong><br />

For the introduction of <strong>GPS</strong> broadcast navigation messages into the <strong>Bernese</strong> <strong>GPS</strong> <strong>Software</strong><br />

an alternative way is available which represents the standard for earlier versions of the<br />

software and is contained in <strong>Version</strong> <strong>5.0</strong> for assuring backward compatibility: <strong>GPS</strong> RINEX<br />

navigation messages may be converted into the internal broadcast format (default extension<br />

BRD, see Section 22.7.1) using the program RXNBV3 (”Menu>RINEX>Import RINEX to <strong>Bernese</strong> format<br />

>Navigation files”, description in Section 4.3). This file format may only hold broadcast messages<br />

for <strong>GPS</strong> and not for GLONASS.<br />

Let us mention that it is easy to edit the <strong>Bernese</strong> broadcast files with any text editor: files<br />

may be concatenated, separated, and messages deleted. In this context it is important to<br />

know that the messages need not be sorted according to satellites or time. The message<br />

number which is given for each message is ignored by the access routine.<br />

<strong>Bernese</strong> broadcast messages may be checked for inconsistencies using the program<br />

BRDTST (”Menu>Orbits/EOP>Broadcast orbits>Check broadcast orbits”) (see following section). Program<br />

BRDTAB (”Menu>Orbits/EOP>Broadcast orbits>Create tabular orbits”) must then be used to transform<br />

the orbit information from the broadcast message into a set of tabular ephemerides in the<br />

inertial system (we recommend to use the system J2000.0, exclusively). You will have to use<br />

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