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AIDJEX Bulletin #40 - Polar Science Center - University of Washington

AIDJEX Bulletin #40 - Polar Science Center - University of Washington

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The translocation principle removes most <strong>of</strong> the errors external to the<br />

receivers. Still remaining are instrumentation errors at each receiver due<br />

to oscillator and receiver timing errors. For most <strong>of</strong> the main experiment,<br />

the crystal oscillators used in our systems introduced no detectable errors<br />

in our position measurements. However, because <strong>of</strong> inadequate oscillators,<br />

translocation calibration tests before the main experiment produced few useful<br />

data. During the first month, temperature fluctuations <strong>of</strong> a few tenths <strong>of</strong> a<br />

degree Fahrenheit in 10 minutes at the oscillators produced frequency changes<br />

<strong>of</strong> 1 part in lo1 O .<br />

Such a frequency drift will cause fix errors <strong>of</strong> 5-10 m<br />

[Denzler, 19701. Oscillators less sensitive to temperature were used after<br />

the first month.<br />

NavSat receivers used for navigation generally employ the simplification<br />

<strong>of</strong> measuring Doppler counts with respect to time marks transmitted by the<br />

satellite. Errors in decoding these time marks introduce 5-10 m position<br />

errors. Receivers intended for more precise applications eliminate this<br />

source <strong>of</strong> error by adding a stable internal time base to control or correct<br />

Doppler counts. We used such a local clock, derived from the crystal oscillator,<br />

to measure the errors in decoding satellite time marks and to correct<br />

Doppler counts using the algorithm in Appendix A.<br />

RECEIVER CONTROL<br />

There were six NavSat satellites during the experiment, each completing<br />

one orbit every 108 minutes and staying within range <strong>of</strong> high-latitude receivers<br />

for about 18 minutes on each orbit (Fig. 4). Therefore, it commonly occurred<br />

that more than one satellite was within range at the same time. Because our<br />

objectives included the collection <strong>of</strong> data from as many passes as possible<br />

while tracking the same passes at different camps, the standard practice <strong>of</strong><br />

tracking the first satellite within range for as long as possible was not<br />

efficient enough for us. The data collection had to be more selective and<br />

had to employ identical techniques at all camps.<br />

The objective <strong>of</strong> our receiver control procedure was to obtain data from<br />

the entire critical interval <strong>of</strong> as many passes as possible. The procedure<br />

involved logical choices based on predictions <strong>of</strong> Doppler frequencies as a<br />

89

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