Sun Chuang, Ren Shun-Qing, Wang Chang-Hong
Space Control and Inertial Technology Research Center, Harbin Institute of Technology, Harbin 150001, China.
Rev Sci Instrum. 2019 Aug;90(8):085002. doi: 10.1063/1.5089603.
The common error calibration model of a linear accelerometer usually cannot meet the accuracy requirement without considering the influence of misalignments in the precision centrifuge test. In order to improve the calibration accuracy, a series of coordinate systems is established and precise accelerations along the input axes of the accelerometers are deduced first. Then, by analyzing the mechanisms of the main error sources, the revised error calibration model is established which includes the misalignments, the radius errors, and the nonlinearity error terms. Then, the measurement methods are proposed to estimate the initial angular misalignments, the installation angular misalignments, and the installation radius misalignments by a theodolite and the accelerometer themselves in the different modes of the centrifuge, respectively. Finally, the experimental measurement results show that the initial angular misalignments are estimated accurately and less than 0.5' after adjustment. Further investigation shows that the adequacy of the common error calibration model decline obviously and the calibration accuracies are lower than 6 × 10g/g without considering the misalignments. After compensating for the misalignments in the revised model, the error coefficients are identified precisely, and the calibration accuracies are higher than 1.5 × 10g/g.
线性加速度计的常用误差校准模型在不考虑精密离心机测试中不对准影响的情况下,通常无法满足精度要求。为提高校准精度,首先建立了一系列坐标系,并推导了沿加速度计输入轴的精确加速度。然后,通过分析主要误差源的机理,建立了包含不对准、半径误差和非线性误差项的修正误差校准模型。接着,提出了分别利用经纬仪和加速度计自身在离心机不同模式下估计初始角不对准、安装角不对准和安装半径不对准的测量方法。最后,实验测量结果表明,初始角不对准估计准确,调整后小于0.5'。进一步研究表明,不考虑不对准情况时,常用误差校准模型的充分性明显下降,校准精度低于6×10g/g。在修正模型中补偿不对准后,误差系数被精确识别,校准精度高于1.5×10g/g。