Nano-g accelerometers are widely used in the space exploration and measurement of the earth's gravitational field. It is essential to precisely evaluate error effects at high orders such as cross-coupling for applications in a dynamic environment. Nevertheless, it remains challenging to meet the precision requirements using conventional calibration measures. In this paper, we propose a method to separate the cross-coupling coefficients of a linear single-axis accelerometer by mounting it on a steadily rotating rate table that is tilted at a fixed deviation angle with respect to the horizontal plane. The gravity component is periodically modulated along the input axis per revolution. Simultaneously, a series of centripetal acceleration is applied along the cross axis in sequence while adjusting the rotation frequency of the rate table by steps. Thus, the cross-coupling coefficient can be separated by its dependence both on the modulated gravity acceleration and the centripetal acceleration. In comparison with the static multipoint angular rotation test on a tilted dividing head, the proposed dynamic modulation method demonstrates improved robustness against corruption from bias drift, with an improved uncertainty. This method to separate the cross-coupling coefficient is suitable for testing high-resolution accelerometers, without requiring high bias stability or sensitive response sustaining at ultra-low frequency.
INDEX TERMNano-g accelerometer, cross-coupling coefficient, rotation modulation, static multipoint, parameter identification, model equation.
I. INTRODUCTIONAccelerometers with a resolution in the order of magnitude of ng/√Hz (where g ≈ 9.8 m/s 2 denotes the earth's gravity) are important for the exploration of the temporal and spatial variation of gravitational field, providing information on the substance density distribution of our planet 1,2 . The applications range from Earth's crust movement, through resource exploration to gravity-aided navigation 3,4 . In many application scenarios like moving-base gravity measurements, accelerometers are required to resolve acceleration of nano-g or sub nano-g in airborne or shipborne environments with relatively large dynamic noises 5,6 . This requirement is demanding since the severe mechanical vibration of the moving vehicle can easily lead to corrupting effects through non-ideal responses of accelerometers. For example, the principle of the commercial airborne gravity gradiometer is based on measuring the differences between matched pairs of rotating accelerometers. In such a gradiometer, second-order coefficients of a few μg/g 2