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Pre-Phase A Report - Lisa - Nasa

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3.2 The inertial sensor 71<br />

Figure 3.10 Scheme of one channel loop.<br />

to the full scale range of acceleration required for the control of the proof mass. It shall<br />

be changed according to the different operation modes from tens of volts to hundreds of<br />

milli-volts.<br />

A supplementary set of electrodes, called injection electrodes in Figures 3.8, 3.9 and 3.10, is<br />

used to control the proof-mass electrical potential, in particular at the pumping frequency<br />

of the capacitive sensing. This solution has been preferred to a thin gold wire used in<br />

other space accelerometers because of the stiffness and of the damping that the wire may<br />

generate. Experimental investigations have demonstrated that the wire is only compatible<br />

with a resolution of several 10−14 ms−2 / √ Hz at room temperature [86].<br />

3.2.4 Evaluation of performances<br />

The performances of the inertial reference sensor have been evaluated by considering the<br />

geometry and the characteristics of the sensor head, the characteristics of the electronics<br />

configuration and the environment on board the LISA satellite. In particular this last<br />

point leads to a required pressure inside the housing of less than 10−6 Pa.<br />

The evolution of the charge Q of the isolated proof mass is one of the most critical error<br />

sources. On the one hand, the proof mass is subjected to the electrostatic forces appearing<br />

with the image charges on the electrodes in regard to the proof mass; the resultant of<br />

these forces is not null when the configuration is not perfectly symmetric, in particular for<br />

any off-centering of the proof mass with respect to the sensor cage. On the other hand,<br />

this charge Q induces a Lorentz force when it moves in the interplanetary magnetic field.<br />

In fact Q is the sum of the charge acquired when the proof mass separates from the<br />

accelerometer cage at suspension switch-on, and of the charge resulting from the cosmic<br />

particle bombardment, especially from the proton flux over 100 MeV. When considering<br />

achargingrateof10 −17 to 10 −18 C/s [87, 88], the 2×10 −14 C limit required is reached in<br />

less than one hour. Therefore the charge has to be measured exploiting the electrostatic<br />

device itself, and the proof mass has to be discharged, continuously or time by time, for<br />

instance by photo-electric emission induced by ultraviolet light [87].<br />

Other electrostatic-force noises must be considered: they are induced either by the fluc-<br />

Corrected version 2.08 3-3-1999 9:33

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