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磁悬浮控制敏感陀螺角动量包络分析
引用本文:杨洋,王卫杰,汪洲,樊亚洪,薛乐.磁悬浮控制敏感陀螺角动量包络分析[J].北京航空航天大学学报,2022,48(10):2061-2069.
作者姓名:杨洋  王卫杰  汪洲  樊亚洪  薛乐
作者单位:1.航天工程大学 研究生院, 北京 101416
基金项目:国家自然科学基金52075545
摘    要:针对磁悬浮控制敏感陀螺(MSCSG)空间应用问题,研究其多自由度角动量包络模型。依据MSCSG的机械结构,分析磁悬浮转子径向万向偏转特性,明晰MSCSG轴向一个自由度转子转速变化飞轮力矩和径向两自由度转子万向偏转陀螺力矩输出机理。基于洛伦兹力磁轴承(LFMB)原理,分析径向偏转力矩与控制电流的线性关系,揭示MSCSG陀螺力矩高精度高带宽的优势。考虑转子径向偏角和轴向转速饱和问题,基于重构偏角和旋转矩阵构建MSCSG角动量包络模型。仿真分析了MSCSG径向偏转力矩高精度高带宽、轴向飞轮力矩高精度的特性。开展MSCSG偏转力矩高带宽性能测试,实验验证MSCSG能够输出大于100 Hz的径向偏转力矩。研究结果表明,MSCSG具有航天器高动态微振动抑制和高精度姿态控制的空间应用前景。 

关 键 词:磁悬浮控制敏感陀螺(MSCSG)    洛伦兹力磁轴承(LFMB)    角动量包络    力矩包络    高精度高带宽
收稿时间:2021-02-07

Momentum envelope analysis of magnetically suspended control sensitive gyroscope
Institution:1.Graduate School, Space Engineering University, Beijing 101416, China2.Department of Aerospace Science and Technology, Space Engineering University, Beijing 101416, China3.Beijing Institute of Control Engineering, Beijing 100190, China4.The Army 63931, Beijing 100094, China
Abstract:Aiming at engineering application problems, the multi-degree-of-freedom angular momentum envelope model of magnetically suspended control and sensing gyroscope (MSCSG) is studied. Based on the mechanical structure of MSCSG, the characteristics of radial universal deflection of magnetic suspension rotor are analyzed. Axial 1-DOF Flywheel torque and radial 2-DOF gyroscope torque output mechanism of MSCSG are clarified. Based on the Lorentz force magnetic bearing (LFMB) principle, the linear relationship between the radial deflection torque and the control current is analyzed, which reveals the advantages of the MSCSG torque with high precision, high bandwidth and small amplitude. Considering rotor speed saturation, the MSCSG angular momentum envelope model is constructed based on deflection reconstruction and rotation matrix. The simulation shows that although radial deflection torque has a high bandwidth, small amplitude, and axial flywheel torque has a high precision and large magnitude. High bandwidth performance test of the MSCSG deflection torque is carried out, showing that MSCSG can output radial deflection torque whose frequency is greater than 100 Hz. It is shown that MSCSG has the prospect of strong micro-vibration suppression under high dynamic conditions and high precision attitude control. 
Keywords:
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