2023
DOI: 10.1007/s00190-023-01716-2
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Impacts of frequency-dependent instrument noise for next-generation gravimetric mission on determining temporal gravity field model

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Cited by 3 publications
(1 citation statement)
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“…In this paper, we have designed a 70 g-TM accelerometer with minimum size and mass with improved resolution. The following three operating modes are obtained by changing the bias voltage V b : (1) V b = 0.5 V, the accelerometer resolution is up to 10 −12 m s −2 Hz −1/2 magnitude for satellite gravity gradient measurement; (2) V b = 2.5 V, the accelerometer provides a resolution of 10 −11 m s −2 Hz −1/2 for satellite tracking measurement [16]; (3) V b = 25 V, the accelerometer has 10 −10 m s −2 Hz −1/2 resolution and a large measurement range to satisfy the needs of other special experimental tests. The in-orbit performance of the 70 g-TM accelerometer was tested on the Tianqin-1 (TQ-1) satellite launched in 2019, and the measured residual acceleration is about 2.0 × 10 −11 m s −2 Hz −1/2 at 0.04 Hz.…”
Section: Introductionmentioning
confidence: 99%
“…In this paper, we have designed a 70 g-TM accelerometer with minimum size and mass with improved resolution. The following three operating modes are obtained by changing the bias voltage V b : (1) V b = 0.5 V, the accelerometer resolution is up to 10 −12 m s −2 Hz −1/2 magnitude for satellite gravity gradient measurement; (2) V b = 2.5 V, the accelerometer provides a resolution of 10 −11 m s −2 Hz −1/2 for satellite tracking measurement [16]; (3) V b = 25 V, the accelerometer has 10 −10 m s −2 Hz −1/2 resolution and a large measurement range to satisfy the needs of other special experimental tests. The in-orbit performance of the 70 g-TM accelerometer was tested on the Tianqin-1 (TQ-1) satellite launched in 2019, and the measured residual acceleration is about 2.0 × 10 −11 m s −2 Hz −1/2 at 0.04 Hz.…”
Section: Introductionmentioning
confidence: 99%