TPF-C Technology Plan - Exoplanet Exploration Program - NASA
TPF-C Technology Plan - Exoplanet Exploration Program - NASA
TPF-C Technology Plan - Exoplanet Exploration Program - NASA
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Chapter 4<br />
(5) The Fine Steering Mirror (FSM) and Fine Guidance Sensor (FGS) are key to the pointing.<br />
The FSM will demonstrate small angle jitter reduction and high accuracy pointing control, in<br />
tandem with the FGS focal plane detector measurements and centroiding algorithm. The focal<br />
plane is included for demonstration of centroiding accuracy, bandwidth (frame rate), and<br />
measurement noise characteristics. The end-to-end performance of the FGS/FSM will need to<br />
demonstrate the centroiding algorithm. The focal plane can demonstrate separately centroiding<br />
accuracy, bandwidth (frame rate), and measurement noise characteristics. The end-to-end<br />
performance of the FGS/FSM will need to demonstrate ~1/300 λ/D centroiding performance as<br />
defined by contrast requirements.<br />
(6) Because of the reliance on image shape, a simulation of FGS optical path will be used to<br />
produce a simulation of the “spot.” This includes the key reference surfaces (such as the<br />
reflection off the coronagraph spot), or diffraction pick-off locations used to pick off the science<br />
reference star signal. This will be used as part of the test with the FGS. This test may require<br />
copies of particular surfaces, including any substrates used as reflecting surfaces.<br />
(7) Isolation of testbed from acoustics and external vibration. This will require both a vacuum<br />
and isolation of key testbed components for full demonstration, which may be too expensive for<br />
this size testbed; a reduced approach would test the FSM and FGS separately in an isolated<br />
vacuum chamber and use measured performance to evaluate overall performance.<br />
The entire spacecraft would be required for full testing. Since this is not feasible, individual<br />
components will be tested in a reduced testbed. The ACS of the S/C and coronagraph is as shown<br />
in Figure 4-14. The testbed, shown in figures 4-13 and 4-15, introduces realistic disturbances and<br />
incorporates key components and measurement (for performance validation) devices.<br />
Progress to Date<br />
This testbed is currently in the requirements definition and planning stage. No other resources<br />
have been allocated for this particular testbed activity up to this time. Detailed design work for<br />
the testbed is scheduled to begin near the end of Phase A.<br />
Figure 4-14. Simplified ACS diagram.<br />
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