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Precise Orbit Determination of Global Navigation Satellite System of ...

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Chapter 4 Major Error Sources <strong>of</strong> <strong>Satellite</strong> Observations<br />

Pseudorange Error(m)<br />

Pseudorange Errors(m)<br />

80<br />

60<br />

40<br />

20<br />

0<br />

-20<br />

-40<br />

-60<br />

-80<br />

25<br />

20<br />

15<br />

10<br />

5<br />

0<br />

-5<br />

-10<br />

-15<br />

-20<br />

-25<br />

0 50 100 150 200 250 300 350 400 450<br />

M ultipath De lay(m )<br />

Figure 4-2 Multipath Error Envelope for GPS Code Pseudoranges<br />

38<br />

C/A Code<br />

P Code<br />

0 50 100 150 200 250 300 350 400 450 500 550 600<br />

M u ltip a th D e la y (m )<br />

Figure 4-3 Periodic Function <strong>of</strong> Multipath Error<br />

4.2.2 Influence <strong>of</strong> Multipath Errors on Range and Phase Observations<br />

From the mathematical point-<strong>of</strong>-view, the influence <strong>of</strong> multipath delay δ on correlation time τ ′ can be directly<br />

derived from auto-correlation function R( τ ) .<br />

Using very simple signal equation, suppose the arrived signal from satellite is<br />

S d<br />

= A cosω ( t −τ<br />

)<br />

where<br />

τ time delay from the satellite to the receiver<br />

One multipath signal reflected from near object is:<br />

S m<br />

= αA cos[ ω(<br />

t −τ<br />

−δ<br />

)]<br />

C/A<br />

P<br />

(4-31)<br />

= α A cos[ ω(<br />

t −τ<br />

) + θ m ]<br />

(4-32)<br />

where<br />

α multipath relative amplitude coefficient < 1;

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