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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 />

74

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