15 citations as recorded by crossref.

1. Mission design aspects for the mass change and geoscience international constellation (MAGIC) B. Heller-Kaikov et al. https://doi.org/10.1093/gji/ggad266
2. GRACE Accelerometers Sensitive to Ionosphere Plasma Waves: Similarities between Twangs and Whistlers A. Schlicht https://doi.org/10.3390/geosciences12060228
3. Benefit of enhanced electrostatic and optical accelerometry for future gravimetry missions A. Kupriyanov et al. https://doi.org/10.1016/j.asr.2023.12.067
4. An ultra-high sensitivity 70 g-TM electrostatic accelerometer for next generation satellite gravity measurement A. Zhou et al. https://doi.org/10.1088/1361-6382/acf08a
5. Noise limit of a torsion pendulum under optomechanical control Y. Tan et al. https://doi.org/10.1103/PhysRevA.92.032131
6. Enhanced onboard side-lobe GNSS orbit determination for LuTan-4A IGSO satellite with accelerometer data R. Mu et al. https://doi.org/10.1016/j.measurement.2025.117460
7. Increasing the dynamic range of electrostatic accelerometers by adjusting the zero-position J. Zhou et al. https://doi.org/10.1088/1361-6501/ade5c3
8. Tilt-to-Length Coupling in the GRACE Follow-On Laser Ranging Interferometer H. Wegener et al. https://doi.org/10.2514/1.A34790
9. Impact of tone errors in future satellite gravimetry missions N. Pfaffenzeller et al. https://doi.org/10.1016/j.asr.2025.02.059
10. Demonstration on the Optimal Design of Resolution Indexes of High and Low Sensitive Axes from Space‐Borne Accelerometer in the Satellite‐to‐Satellite Tracking Model https://doi.org/10.1002/cjg2.1446
11. Flight performance analysis of GRACE K-band ranging instrument with simulation data J. Kim & S. Lee https://doi.org/10.1016/j.actaastro.2009.04.010
12. Physical Explanation on Designing Three Axes as Different Resolution Indexes from GRACE Satellite-Borne Accelerometer Z. Wei et al. https://doi.org/10.1088/0256-307X/25/12/084
13. Responses of Thermospheric Mass Densities to the October 2016 and September 2017 Geomagnetic Storms Revealed From Multiple Satellite Observations R. Li & J. Lei https://doi.org/10.1029/2020JA028534
14. Estimation of non-gravitational acceleration difference between two co-orbiting satellites using single accelerometer data J. Kim & B. Tapley https://doi.org/10.1007/s00190-015-0796-2
15. Precise real-time orbit determination for LEO satellites using accelerometer data as observations R. Zhang et al. https://doi.org/10.1016/j.asr.2026.05.070