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Antti Lehtinen Doppler Positioning with GPS - Matematiikan laitos

Antti Lehtinen Doppler Positioning with GPS - Matematiikan laitos

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the receiver needed to collect measurement data over several minutes. The actual<br />

computation of the receiver position was based on the <strong>Doppler</strong> curve of a satellite<br />

pass. <strong>Doppler</strong> curves of satellites are flatter than in Figure 2.2. This is because<br />

they travel alongcircular orbits rather than straight lines. The position of the<br />

receiver was determined by curve fitting. The latitude and longitude estimates<br />

were optimised such that the computed <strong>Doppler</strong> curve fitted to the measured<br />

data. The computational details can be found in [Laurila, p. 474]. The accuracy<br />

of the Transit system was about half a kilometre.<br />

In order to compute the <strong>Doppler</strong> curves, one also needs to know the position<br />

and velocity vectors of the satellite. Thus, the Transit satellites transmitted<br />

binary data by phase modulation. This data is called ephemeris. One was able<br />

to compute the satellite position and velocity from the ephemeris. The Transit<br />

satellites transmitted continuous wave signals on two distinct frequencies, namely<br />

150 MHz and 400 MHz. The purpose of this was to eliminate the first order<br />

ionospheric refraction and receiver frequency measurement errors. The accuracy<br />

of the Transit system was about 100 meters for a stationary receiver, but was<br />

severely worse for a receiver in unknown motion [Laurila, p. 476]. According<br />

to [Parkinson & Spilker, p. 4], the Transit system is still operational, but new<br />

satellites are not beinglaunched.<br />

6

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