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Antti Lehtinen Doppler Positioning with GPS - Matematiikan laitos

Antti Lehtinen Doppler Positioning with GPS - Matematiikan laitos

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Chapter 4<br />

<strong>Doppler</strong> <strong>Positioning</strong> <strong>with</strong> the<br />

<strong>GPS</strong><br />

In this chapter, the possibility of usingthe <strong>Doppler</strong> measurements in <strong>GPS</strong> will<br />

be discussed. The theory for positioningbased on simultaneous <strong>Doppler</strong> measurements<br />

will be developed. In addition, an iterative algorithm suitable for the<br />

positioningis presented.<br />

4.1 Need for <strong>Doppler</strong> <strong>Positioning</strong><br />

The Global <strong>Positioning</strong> System was developed for pseudorange positioning. There<br />

is no doubt that usingthe pseudorange measurements is the most accurate way<br />

to find a position estimate for the receiver. However, the end of the preceding<br />

chapter gave a glimpse of the difficulties that frequently arise in pseudorange<br />

positioning.<br />

Very often it happens, that there are several attenuated <strong>GPS</strong> satellite signals<br />

available. The signals are so noisy that the demodulation of the navigation message<br />

is impossible. Thus, the pseudorange measurements cannot be performed.<br />

However, the signals are sufficiently good so that the signals can be recognised<br />

accordingto the PRN codes. In addition, the received signal frequencies can be<br />

measured. The frequency differences are mainly caused by the <strong>Doppler</strong> effect. In<br />

this chapter it will be shown that the frequency shifts can be used for positioning<br />

<strong>with</strong>out knowledge of the pseudoranges. This kind of positioning will be referred<br />

to as <strong>GPS</strong> <strong>Doppler</strong> positioning.<br />

In pseudorange positioning the user needs to know the satellite positions. In<br />

<strong>GPS</strong> <strong>Doppler</strong> positioningthe same applies, but the user also needs to know the<br />

satellite velocities. The usual way to achieve this information is to demodulate the<br />

16

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