DGCMG框架伺服系统摩擦力矩建模及辨识
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TP275; V448; TH132

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国家自然科学基金资助项目(61203112)


Analysis of Friction Torque Model of DGCMG Gimbal Servo Systemwith Its Identification
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    摘要:

    为了减小强陀螺效应条件下双框架控制力矩陀螺(double gimbal control moment gyroscope,简称DGCMG)框架伺服系统的非线性摩擦力矩对框架伺服系统控制精度的影响,提出了一种对DGCMG框架伺服系统非线性摩擦力矩精确建模和辨识的方法。分析了DGCMG框架伺服系统的动力学方程,在研究内、外框架摩擦力矩随内外框架角速度和陀螺力矩变化规律的基础上,建立了内、外框架摩擦力矩精确的数学模型,并用控制力矩陀螺的实际参数和实验采集数据对摩擦力矩模型参数进行了遗忘因子递推最小二乘法辨识。实验结果验证了所建模型的正确性和辨识结果的准确性,有助于补偿DGCMG框架伺服系统的非线性摩擦力矩,提高框架伺服系统的控制精度。

    Abstract:

    The nonlinear friction torque of the double gimbal control moment gyroscope (DGCMG) gimbal servo system heavily influences its control precision with a gyroscopic effect. In order to alleviate this issue, a method of creating an accurate friction torque modeland identifying its parameters are presented. The dynamics of the CMG gimbal servo system are analyzed. Based on the study of the friction torque in inner and outer gimbals which are related to gimbal′s angle velocity and gyro torque, an accurate model of friction torques in the inner and outer gimbals has been established. Then, using the forgetting factor recursive least square (FFRLS) method, the parameters of this model are identified using the real coefficients of the CMG and experimental sampling data. The accuracy of the friction models and the identification results are validated through experiments, which serves to compensate the nonlinear friction torque of DGCMG gimbal servo system and improve the control precision of the gimbal servo system.

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  • 在线发布日期: 2015-01-06
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