# On-Ground Calibration of a Nano-G Accelerometer for Micro-Vibration Monitoring in Space on a Dual-Axis Indexing Device

**Authors:** Yang Zhou, Zhi Li, Qiangwei Xu, Xiangchun Li

PMC · DOI: 10.3390/s25206289 · Sensors (Basel, Switzerland) · 2025-10-10

## TL;DR

This paper presents a method to accurately calibrate a highly sensitive accelerometer for space use by rotating it on a dual-axis device to improve calibration precision.

## Contribution

A novel on-ground calibration procedure for nano-g accelerometers using a dual-axis indexing device to correct for tilt and higher-order gravity effects.

## Key findings

- Accelerometer bias errors were reduced to ±2% and scale factor errors to ±0.01 mg.
- All three accelerometer units were aligned into a unified coordinate frame for consistent measurements.
- Calibration results showed consistency with collocated accelerometers during a space mission.

## Abstract

High-sensitivity accelerometers are essential for spacecraft micro-vibration monitoring. This study proposes a procedure to facilitate precise on-ground calibration of such accelerometers with a limited operational range by rotating to multiple positions with its input axis mounted along the horizontal tilt axis of a two-axis indexing device. Each single-axis accelerometer unit of a self-developed tri-axial nano-g accelerometer was respectively tested with its various reference axes along the rotation axis for identifying the parameters of their model equations including higher-order terms. The minute tilt axis deviation of the test equipment from the horizontal plane and the accelerometer’s higher-order response to gravity during calibration are corrected for application in the microgravity environment. Errors of accelerometer biases and scale factors are satisfactorily improved, respectively, to ±2% and ±0.01 mg, by at least one order of magnitude. Parameters of all three units of the accelerometer are unified into one coordinate frame defined by the accelerometer mounting surface. Acceleration measured by our accelerometer shows consistency with the other collocated one in a space mission.

## Full-text entities

- **Diseases:** OA (MESH:C566610), MEMS-M3 (MESH:D015473), injury to (MESH:D014947)
- **Species:** Homo sapiens (human, species) [taxon 9606]
- **Cell lines:** MEMS — Homo sapiens (Human), Neuraminidase deficiency, Induced pluripotent stem cell (CVCL_YT44)

## Full text

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## Figures

18 figures with captions in the complete paper: https://tomesphere.com/paper/PMC12568062/full.md

## References

39 references — full list in the complete paper: https://tomesphere.com/paper/PMC12568062/full.md

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Source: https://tomesphere.com/paper/PMC12568062