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Bernese GPS Software Version 5.0 - Bernese GNSS Software

Bernese GPS Software Version 5.0 - Bernese GNSS Software

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17.9 Low Earth Orbiters<br />

17.9 Low Earth Orbiters<br />

The simulation of <strong>GNSS</strong> observations for a Low Earth Orbiter is basically the same as for<br />

a terrestrial station. Only some input files and settings call for special attention.<br />

The important differences for the simulation of <strong>GNSS</strong> observations for LEOs are listed<br />

below:<br />

(1) Although a LEO has no defined station coordinates its name must appear in the<br />

coordinate file in panel “<strong>GPS</strong>SIM 1: Filenames” with the same name as in the “Satellite<br />

information” file (panel “<strong>GPS</strong>SIM 1.1: General Files”). The coordinates of the LEO are of<br />

no importance and may even be zero.<br />

(2) The LEO must be listed in section TYPE 005 of the “Station information”-file (panel<br />

“<strong>GPS</strong>SIM 1.1: General Files”) with marker type SPACEBORNE. If the keyword SPACE-<br />

BORNE is missing program <strong>GPS</strong>SIM interprets the LEO as a ground based station.<br />

(3) Option “LEO-files” in the first panel must be checked in order to display the LEOspecific<br />

panel “<strong>GPS</strong>SIM 1.2: LEO Options”.<br />

(4) You need either a LEO standard orbit file or a file with kinematic coordinates to define<br />

the trajectory of the low satellite.<br />

(5) If you have specified “Kin. input coordinates” in the first panel you may select a file<br />

containing kinematic velocities in panel “<strong>GPS</strong>SIM 1.2: LEO Options”. This information<br />

is used to define the local orbit frame needed to compute the satellite’s attitude.<br />

Alternatively you can specify a “LEO attitude” file. The attitude is necessary to apply<br />

antenna offsets.<br />

If the LEO trajectory is obtained from a standard orbit, no velocity file is required.<br />

An attitude file may be used, though.<br />

(6) No troposphere model is applied for low Earth satellites. The option “ZPD model and<br />

mapping function” in “<strong>GPS</strong>SIM 3.2: Simulation Options” is ignored.<br />

(7) The modeling of the ionosphere should be deactivated.<br />

(8) The a priori sigmas and the “Elevation-dependent sigmas” checkbox are separately available<br />

for LEOs in panel “<strong>GPS</strong>SIM 3.4: Simulation Options”.<br />

17.10 Applications for Simulated Data<br />

Simulated data can be used in a number of different ways. Most of the applications, however,<br />

may be assigned to one of the following three main categories:<br />

Verifying software algorithms: A well defined set of simulated observation data can be helpful<br />

while testing the correct implementation of software algorithms. The testing procedure<br />

profits from the fact that, as opposed to real data, the correct results (e.g., number<br />

of cycle slips) are known a priori.<br />

Pre-analyses: Satellite scenario, network layout, statistical properties, and systematic errors<br />

are known for simulated data. Thus one may study the expected quality of the results<br />

depending on different processing strategies and option settings. A pre-analysis makes<br />

sense, e.g., to learn what to expect from a planned campaign or how to design a new<br />

campaign to get optimal results.<br />

<strong>Bernese</strong> <strong>GPS</strong> <strong>Software</strong> <strong>Version</strong> <strong>5.0</strong> Page 353

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