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PhD thesis - Institute for Space Research - University of Calgary

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164 C: Attitude Solution<br />

Figure C.2: Same as Figure C.1 but <strong>for</strong> the Y components.<br />

Figure C.3: Same as Figure C.1 but <strong>for</strong> the Z components (spin-axis, parallel<br />

to B 0. The science magnetometer data and model fit have both have a<br />

quadratic subtracted to make the differences easier to see.

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