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LISA Pathfinder test mass injection in geodesic motion: status of the on-ground testing

机译:测地运动中的LISA Pathfinder测试质量注射:地面测试的状态

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The LISA Technology Package (LTP) onboard the LISA Pathfinder mission aims to demonstrate, in orbit, several critical technology milestones for LISA, including the purest geodesic motion ever achieved for a macroscopic body. The gravitational reference sensor in the LTP hosts a heavy test mass (TM) surrounded by electrodes, at a relatively large 'gap' distance of several mm, which are used to measure and control the TM position and attitude. The large gaps-necessary to minimize the force noise acting on the TM-limit the available level of electrostatic actuation force that can be applied to the TM and thus the authority to control its position and velocity. Due to the large mass and gaps, a caging mechanism is required to securely hold the TM during the launch phase, when the whole payload endures large accelerations. Later in orbit, the TM must be injected into its geodesic trajectory, through the release from the caging mechanism and subsequent capture by the electrostatic actuation. During the release phase, the constraining device must limit adhesion forces that exert a net impulse upon rupture, such that the required forces needed to control the TM do not exceed the actuation authority. The TM injection into geodesic motion, and most critically the release phase, constitutes a potential point of failure for the mission. The on-ground verification of this phase is performed by measuring the momentum transferred between TM-representative surfaces and the release device, reproducing the dynamics that will take place in flight. This paper reports on the testing activities performed at the Department of Mechanical and Structural Engineering of the University of Trento.
机译:LISA探路者任务中的LISA技术包(LTP)旨在在轨道上展示LISA的几个关键技术里程碑,包括有史以来对宏观物体实现的最纯净的测地运动。 LTP中的重力参考传感器承载着被电极围绕的较重测试质量(TM),相对较大的“间隙”距离为几毫米,用于测量和控制TM的位置和姿态。为了使作用在TM上的力噪声最小化所需的较大间隙限制了可施加到TM的静电致动力的可用水平,从而限制了控制其位置和速度的权限。由于较大的质量和间隙,当整个有效载荷承受较大的加速度时,在发射阶段需要使用笼式机构来牢固地保持TM。在轨道的后期,必须通过从笼式机构释放并随后通过静电致动捕获,将TM注入其测地线轨迹。在释放阶段,约束装置必须限制在破裂时施加净脉冲的粘附力,以使控制TM所需的力不会超过操纵权限。将TM注入测地运动中,最关键的是释放阶段,构成了任务的潜在失败点。通过测量TM代表表面与释放装置之间传递的动量来执行此阶段的地面验证,从而再现将在飞行中发生的动力学。本文报告了特伦托大学机械与结构工程系进行的测试活动。

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