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ETTC'2003 - SEE

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GPS time binary data is about 1ms, a time interval counter is needed in the ground station. Considering<br />

the equipment complexity and working toward minimum parts cost, the clock frequency of the time<br />

interval counter is 200MHz. The ground station clock quantification error ε q is 5ns.<br />

4) Telemetry receiver ε d<br />

The error ε d resulted from the telemetry receiver is affected by the selection of the telemetry system.<br />

In the PCM system, ε d is about one fiftieth of the chip width. If the bit rate is 2Mbps, ε d is about<br />

10ns. In the PPK (Pulse Position Keying) system, ε d is affected by the signal pulse jitter ε t , the<br />

pulse delay resulted by the signal level change ∆ tds<br />

, the pulse delay resulted by the difference of the<br />

'<br />

decision level ∆tds and the RF pulse jitter σ df .<br />

ε t = tr S N<br />

(4)<br />

where tr is the rise time of the pulse signal, S N is the square root of the receiver’s<br />

Signal-to-Noise. For the reliability of the transferred data, the S/N is about 16dB to 17dB. Then<br />

1<br />

ε t = tr<br />

(5)<br />

7<br />

In general, the relationship between the system bandwidth and the rise time is = 0.<br />

5 B .<br />

rt ( k −1)<br />

r 1<br />

∆ tds<br />

=<br />

(6)<br />

k1<br />

where r is the relative decision level, k is the ratio of the actual signal level to the ideal one.<br />

2 , ∆t = 0.<br />

5rt<br />

. = 0.<br />

6 ,<br />

1 = k ds<br />

r<br />

1<br />

∆ t = 0.<br />

3t<br />

. It means that if the actual signal level is twice larger<br />

r ds r<br />

than the ideal one, ∆tds is three times larger than ε t . For this reason, the system gain should be well<br />

controlled to keep the received signal level invariable.<br />

'<br />

∆tds = rtr<br />

k −1)<br />

(7)<br />

( 2<br />

where k is the ratio of the changed decision level to the original one. If the decision level changed<br />

2<br />

10%, then 2 1.<br />

1 , . The error<br />

= k '<br />

∆tds ≈ 0.<br />

42ε<br />

t ε d resulted from the telemetry receiver in one<br />

ground station is<br />

ε = ε + ∆t<br />

+ ∆t<br />

+ σ<br />

(8)<br />

d<br />

2<br />

t<br />

2<br />

ds<br />

In the 3∆t system, the ground stations receive the same telemetry signal and calculate the target’s<br />

position by using the time difference of arrival. The RF pulse jitter contributes nothing. The ε t , ∆ tds<br />

'<br />

and ∆t<br />

of each ground station are independent, then in determining the time difference these errors<br />

ds<br />

will be enlarged. The error<br />

ε d is<br />

'2<br />

ds<br />

2<br />

df<br />

2 2 '2<br />

ε d = 2ε t + 2∆t<br />

ds + 2∆t<br />

ds<br />

(9)<br />

If the bandwidth of PPK system is 9MHz, r = . 6,<br />

k = 2,<br />

k = 1.<br />

1 , S N is about 16dB to<br />

17dB, ≈ 56ns<br />

, ≈ 8ns<br />

t r<br />

5) Doppler shift ε<br />

f<br />

ε , ≈ 16.<br />

8ns<br />

t<br />

t ds<br />

0 1 2<br />

∆ , ∆ 3.<br />

36ns<br />

,<br />

t r<br />

'<br />

tds ≈ d ≈ 26.<br />

7ns<br />

ε 。

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