Calibration of high accuracy accelerometers for ESA missions BepiColombo and JUICE at INRIM

Abstract

High sensitive triaxial accelerometers are used in several space missions to measure the non-gravitational accelerations acting on the spacecraft. Among these, the capacitive accelerometers developed for ESA missions JUICE and BepiColombo were designed to measure accelerations of the order of 3∙10-6 m/s2 with an accuracy level of 300 ppm in the frequency range (3·10-5 - 0.1) Hz. Despite the signal to be be measured is of the same order of magnitude of the seismic noise on the earth, an accurate on-ground calibration is needed.
The facility set-up at INRIM to this purpose is based on a simple principle: the base of the accelerometer is dinamically tilted by an angle α so that the sensor undergoes a component of the gravitational acceleration g proportional to angle α. In practice, several issues have to be addressed by the calibration facility, such as the seismic noise limiting the signal-to-noise ratio, the generation and the accurate measurement of the tilt angle. Furthermore, the calibration was performed taking into account different on-flight conditions such as different operating temperatures and possible deformation of the accelerometers during the launch. The experimental set-up and the calibration procedure are described in the paper. The measurement results and the uncertainty budget show that a relative accuracy of 240 ppm has been achieved.

Test mass charge estimation for the space inertial sensor with extended Kalman filter

“…Spaceborne detectors are more sensitive to gravitational waves in the medium and low frequency bands than ground detectors. In spaceborne gravitational wave detection tasks, a free-floating test mass (TM) in space inertial sensor is used as a mirror of the high-precision intersatellite laser interferometer to provide the inertial reference for the interferometer [15,16]. There are strict requirements for residual TM acceleration noise [17].…”