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MISSION PLAN - PDS Small Bodies Node

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6.2.5 Nucleus Tracking<br />

Given the delivery uncertainty and associated probabilities described in the previous<br />

section, imaging of Wild-2 could be accommodated adequately until E-3 minutes.<br />

However, in order to capture the highest resolution images, obtainable only after E-3<br />

minutes, some action must be taken. As mentioned above, mirror control, centroiding<br />

and the roll maneuver are used to maintain the nucleus within the camera field-of-view.<br />

Centroiding uses selected images (maximum of once every 10 seconds which is<br />

equivalent to every other image after E-4 minutes) and a 1-D algorithm to compute the<br />

mirror correction required to place the comet back into the center of the field-of-view of<br />

the camera. Designed to provide 180° in-plane tracking of Wild-2, this mirror slewing<br />

will compensate for the in-plane and time-of-flight delivery errors. Mirror control and<br />

centroiding are planned to start at E-50 minutes when the comet nucleus is about 3x3<br />

pixels in size. Centroiding is planned to end at closest approach while mirror control is<br />

planned to end at E+20 minutes to support Post Encounter “fill memory” imaging.<br />

To correct the out-of-plane delivery error, a correction must be made along the spacecraft<br />

y-axis. A roll maneuver about the x-axis is planned only once and implemented only if<br />

and when the nucleus image is expected to escape the camera field-of-view. In order to<br />

maintain a real-time telemetry link as long as possible into the encounter, it is desirable to<br />

have this maneuver not occur until absolutely necessary. Current estimates place the<br />

execution of this maneuver between E-4 to -3 minutes. The maneuver is expected to take<br />

no more than a minute to implement including time for attitude stabilization. Figure 6.2-<br />

4 shows the expected roll angle as a function of out-of-plane error and flyby distance. If<br />

a roll maneuver is performed, once the encounter is over, at about E+3 minutes, a<br />

subsequent roll maneuver is performed in order to re-establish communications as soon<br />

as possible.<br />

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