arXivDaily arXiv每日学术速递 周一至周五更新
arXiv 2012.11232physics.ins-detastro-ph.IMgr-qc
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MICROSCOPE仪器描述和确认

MICROSCOPE instrument description and validation

Françoise Liorzou, Pierre Touboul, Manuel Rodrigues, Gilles Métris, Yves André, Joel Bergé, Damien Boulanger, Stefanie Bremer, Ratana Chhun, Bruno Christophe, P… 展开作者

Françoise Liorzou, Pierre Touboul, Manuel Rodrigues, Gilles Métris, Yves André, Joel Bergé, Damien Boulanger, Stefanie Bremer, Ratana Chhun, Bruno Christophe, Pascale Danto, Bernard Foulon, Daniel Hagedorn, Emilie Hardy, Phuong-Anh Huynh, Claus Lämmerzahl, Vincent Lebat, Meike List, Frank Löffler, Benny Rievers, Alain Robert, Hanns Selig

摘要:

为显微镜飞行任务研制了专用加速度计,同时考虑到卫星上测量的加速度的具体范围。考虑到一个微g甚至更小的仪器的整个范围,导致一个定制的概念和高性能的电子检测和伺服驱动的加速度计测试质量。除了一个非常精确的几何传感器核心,高性能的电子架构提供了微弱的静电力和扭矩施加到测试质量的测量。一组电容传感器提供的位置和姿态的测试质量相对于一个非常稳定的黄金涂层笼在二氧化硅。施加在每个测试质量周围的电极上的电压被精细地控制,以产生足够的电场,从而产生测试质量上的静电压力。该磁场使测试质量块相对于仪器结构保持静止。数字控制法的实施,以使仪器操作的灵活性和弱的位置传感器噪声。这些电子设备既为MICROSCOPE的广义相对论测试提供科学数据,也为卫星的无阻力和姿态控制系统(DFACS)提供数据。

英文摘要:

Dedicated accelerometers have been developed for the MICROSCOPE mission taking into account the specific range of acceleration to be measured on board the satellite. Considering one micro-g and even less as the full range of the instrument, leads to a customized concept and a high performance electronics for the sensing and servo-actuations of the accelerometer test-masses. In addition to a very accurate geometrical sensor core, a high performance electronics architecture provides the measurement of the weak electrostatic forces and torques applied to the test-masses. A set of capacitive sensors delivers the position and the attitude of the test-mass with respect to a very steady gold coated cage made in silica. The voltages applied on the electrodes surrounding each test-mass are finely controlled to generate the adequate electrical field and so the electrostatic pressures on the test-mass. This field maintains the test-mass motionless with respect to the instrument structure. Digital control laws are implemented in order to enable instrument operation flexibility and a weak position sensor noise. These electronics provide both the scientific data for MICROSCOPE's test of General Relativity and the data for the satellite drag-free and attitude control system (DFACS).

机构、总结、中文摘要均由AI分析而来,可能存在错误,请以论文正文为准。

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