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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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some redundancy. Four points were used in the central <strong>AIDJEX</strong> array: three<br />

camps (Caribou, camp 1; Blue Fox, camp 2; Snow Bird, camp 3) initially forming<br />

a triangle 100 km on a side with a fourth camp (Big Bear, camp 0) in the<br />

center.<br />

Typically, sea ice moves about 2 km in 12 hours (Fig. 1). Thus, measurements<br />

<strong>of</strong> geographical position accurate to 100 m or better will resolve the<br />

motion quite well. However, the relative position <strong>of</strong> one camp with respect to<br />

another typically changes by about one quarter <strong>of</strong> one percent <strong>of</strong> the distance<br />

between them. For camps 100 km apart, then, typical changes in relative positions<br />

are 250 m in 12 hours (Fig. 2). The design criterion for the positioning<br />

system was set at 510 m for relative positions.<br />

Estimates <strong>of</strong> ice motion were required to support other parts <strong>of</strong> the <strong>AIDJEX</strong><br />

field program, but the requirements did not make the sampling and accuracy<br />

criteria more severe. Briefly stated, these other requirements were: to<br />

provide geographical reference for the meteorological and oceanographic observations;<br />

to correct ocean current measurements by removing the velocity <strong>of</strong> the<br />

ice itself; to correct measurements <strong>of</strong> ice tilt by accounting for the acceleration<br />

<strong>of</strong> the ice; and to support aircraft and submarine operations.<br />

SYSTEM DESIGN<br />

In defining the system configuration we sought to combine high reliability<br />

with low maintenance and repair, improve accuracy in distance measurement,<br />

have automatic operation with standardized selection and acquisition <strong>of</strong> the<br />

maximum number <strong>of</strong> passes, obtain measurements <strong>of</strong> floe rotation, and keep costs<br />

as low as possible. Figure 3 is a block diagram <strong>of</strong> the NavSat equipment<br />

installed at each <strong>of</strong> the four camps. Hardware details are given by Wasilew<br />

and Vivian [1976].<br />

Simple, redundant, commercially proven hardware was used to achieve our<br />

objectives <strong>of</strong> reliability and low cost. Spare components for major systems<br />

were kept at the main camp so that a system could be repaired quickly by<br />

replacing an entire component. We sacrificed some geographic accuracy by<br />

using single-channel (400 MHz) receivers which cannot correct for refraction<br />

effects. On the other hand, because <strong>of</strong> the low cost <strong>of</strong> single-channel<br />

85

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