meetings - Space Flight Mechanics Committee
meetings - Space Flight Mechanics Committee
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