一种新型陀螺的力矩器非圆性误差补偿方法

为提高磁悬浮控制敏感陀螺（MSCSG）对陀螺载体姿态的敏感精度，基于其洛伦兹力磁轴承（LFMB）的设计结构，提出了一种力矩器非圆性误差补偿方法。首先，针对一种新型双球形包络面转子MSCSG，介绍了MSCSG的结构特点与陀螺载体姿态角速度敏感原理，并分别建立了MSCSG力矩器半径误差模型、转子偏转干扰力矩模型与陀螺载体姿态角速度敏感误差模型。其次，通过实验测量了力矩器的圆度，通过MATLAB进行数据拟合得到了力矩器的非圆特性，采用勒让德多项式级数对力矩器非圆性进行了描述，并有效补偿了因力矩器非圆性误差导致的姿态角速度敏感误差。最后，对误差补偿效果进行了仿真验证，结果表明该补偿方法使陀螺载体姿态角速度敏感误差降低了83.5%。此外，本文方法还可以解决LFMB陀螺的相关共性问题。

A new gyro torquer' s non-circular error compensation method

Based on the structural design of the Lorentz force magnetic bearing (LFMB), a kind of torquer's non-circular error compensation method is put forward to enhance the sensitivity accuracy of magnetically suspended control sensitive gyroscope (MSCSG) to gyro carrier attitude. First, for a new type MSCSG with double spherical envelope rotor, the structure features of MSCSG and the attitude angular velocity measurement principle of the gyro carrier are introduced and the radius error model of MSCSG torquer, the interference torque model of rotor's deflection and the measurement error model of the gyro carrier's attitude angular velocity are set up. Then, the roundness of torquer is measured through the experiment, and data fitting is conducted by MATLAB to obtain the non-circular characteristic of the torquer. The non-circular characteristic is described by Legendre polynomial series, and the measurement error of the gyro carrier's attitude angular velocity caused by the torquer's non-circular error is compensated effectively. Finally, the effect of error compensation is verified by the simulation and the results show that the compensation method makes the measurement error of the gyro carrier's attitude angular velocity reduce by 83.5%. In addition, the proposed method can solve the common problems related to LFMB gyro.