SPIRE Design Description - Research Services
SPIRE Design Description - Research Services
SPIRE Design Description - Research Services
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Draft <strong>SPIRE</strong> <strong>Design</strong> <strong>Description</strong> Document<br />
5.2.1 Nod<br />
The NOD function of the telescope is an operation in which the target source is periodically moved from one<br />
instrument chop position to the other chop position by re-pointing the satellite. The pointing direction will<br />
change in the direction of the chopper throw - see Figure 5-2.<br />
Nod<br />
position<br />
1<br />
Figure 5-2 - Pointing positions for a telescope NOD function. The circles represent the size of the telescope Airy<br />
pattern projected onto the sky. The two nod positions have been offset left and right for clarity.(A1 and B2 are coaligned).<br />
The purpose of nodding is to subtract out the signal offset that will be present at some level due to the fact<br />
that the detector will receive different amounts of ambient background power in the two chop positions. This<br />
offset is likely to be larger than low-level signals to be detected, and may also vary significantly with time<br />
over the course of an observation if the primary mirror has a time-varying temperature gradient in the<br />
chopping direction (Griffin, 1998). Nodding takes out the offset in the following way:<br />
Let S = Source signal OA = Offset signal for beam A OB = Offset signal for beam B<br />
Then if we subtract the total signals measured in the two nod positions, we get<br />
(A1 - B1) - (A2 - B2) = [(S + OA) - OB] - [OA - (S + OB)] = 2S.<br />
A2<br />
B2<br />
5.2.2 Raster<br />
The RASTER Spacecraft Function is a series of fine pointing operations of separated by slews such that the<br />
pointing of the telescope axis moves in a raster pattern. Figure 5-3 shows how the raster pattern will be<br />
constructed.<br />
116<br />
A1<br />
B1<br />
Offset for clarity<br />
Chop<br />
throw<br />
Source