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meetings - Space Flight Mechanics Committee

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hardware. This technique maximizes subsystem performance and provides a design method<br />

to replace traditional, iterative design approaches to sensor placement.<br />

10:45 AAS Sensor Calibration for the MICROSCOPE Satellite Mission<br />

13-482 Hanns Selig, ZARM (Center of Applied <strong>Space</strong> Technology and Microgravity),<br />

University of Bremen<br />

The French drag free satellite mission MICROSCOPE(launch in 2017) will perform a test<br />

of the universality of free fall (Equivalence Principle - EP) to an new level of accuracy. The<br />

payload consists of two sensors, each controlling the free fall of a pair of test masses. The<br />

EP test strongly depends on the rejection of disturbances arising from the coupling and<br />

misalignments of the instrument vectorial outputs. Therefore the performance of the<br />

mission depends on the success of the calibration operations which are planned during the<br />

satellite life in orbit, as well as on ground at the ZARM drop tower.<br />

Page 96<br />

23 rd AAS / AIAA <strong>Space</strong> <strong>Flight</strong> <strong>Mechanics</strong> Meeting

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