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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 />

The orbit programs may be found under the menu item ”Menu>Orbits/EOP”. The orbit part<br />

contains programs for checking and converting broadcast ephemerides and extracting broadcast<br />

clocks, to convert precise orbit information into the <strong>Bernese</strong> standard orbit format, and<br />

to generate precise orbit files starting from standard orbit format. Additional tools for extracting<br />

and converting Earth orientation parameters, for the preparation of satellite clock<br />

information necessary for receiver clock synchronization, for extracting information from<br />

the orbit integration program, and to compare precise orbit files or standard orbit files are<br />

available.<br />

The <strong>Bernese</strong> <strong>GPS</strong> <strong>Software</strong> knows several orbit formats (see Table 5.1). The international<br />

format for exchanging precise orbit information within the IGS is the SP3c format. Reading<br />

routines recognize the new format versions as well as older versions of the precise file format<br />

(SP3, SP2 or SP1). The precise orbit files (default extension PRE 1 ) give geocentric Cartesian<br />

coordinates (in kilometers) of the satellites in an Earth-fixed frame together with satellite<br />

clock information for a table with equidistant epochs (usually 15 minutes). For a description<br />

of the file format see ftp://ftp.igs.org/pub/data/format/sp3.txt or [Remondi, 1989].<br />

See also Sections 4.4 and 4.12.<br />

The <strong>Bernese</strong>-internal tabular orbit files are ASCII files (default extension TAB) containing<br />

Cartesian satellite coordinates (in kilometers) in the inertial frame, tabulated at regularly<br />

spaced epochs. The so-called standard orbit files (default extension STD) are binary files<br />

specifying the position of the satellites in the form of a polynomial representation and<br />

are the result of a numerical integration of the equations of motion. All programs of the<br />

<strong>Bernese</strong> <strong>GPS</strong> <strong>Software</strong> that require <strong>GNSS</strong> orbit information read standard orbit files. Earth<br />

orientation parameters are required for all programs accessing standard orbit files in order<br />

to perform the transformations between the Earth-fixed and the inertial frame. In addition<br />

to the file formats listed in Table 5.1 broadcast information in RINEX and <strong>Bernese</strong> format<br />

can be processed in the <strong>Bernese</strong> <strong>GPS</strong> <strong>Software</strong>.<br />

This chapter first describes how to import and prepare Earth orientation parameters (next<br />

section). Section 5.3 presents the programs available for preparing broadcast information.<br />

Section 5.4 shows how to interpolate precise orbit files and to prepare the orbit information<br />

in the standard orbit format. This is the standard application of the orbit programs in the<br />

<strong>Bernese</strong> <strong>GPS</strong> <strong>Software</strong>. Section 5.5 describes how to extract satellite clock information from<br />

broadcast or precise orbit files, an information which is important to synchronize the receiver<br />

clocks in the data preprocessing step. In the last section the orbit comparison programs are<br />

described. Information on how to estimate orbit and Earth orientation parameters are given<br />

in Chapter 15. For more information on estimating satellite clocks we refer to Chapter 14.<br />

1 In most databases these files have extensions EPH or SP3.<br />

Table 5.1: Important orbit formats used in the <strong>Bernese</strong> <strong>GPS</strong> <strong>Software</strong>.<br />

File Type Format Content, Reference System<br />

PRE Precise Orbit File, SP3 International, ASCII Tabular positions and clocks,<br />

Earth-fixed, geocentric, every 15 min<br />

TAB Tabular Orbit File <strong>Bernese</strong>, ASCII Tabular positions,<br />

inertial, geocentric, every 15 min<br />

STD Standard Orbit File <strong>Bernese</strong>, binary Polynomial representation,<br />

result of numerical integration, inertial,<br />

geocentric<br />

Page 84 AIUB

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