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Calibration Compensation and Accuracy Analysis of Circular Grating Used in Single Gimbal Control Moment Gyroscope

机译:单云台控制力矩陀螺仪用圆光栅的标定补偿和精度分析

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摘要

The accuracy of the circular grating is the key point for control precision of the single gimbal control moment gyroscope servo system used in civilian micro-agile satellites. Instead of using the multi reading heads to eliminate eccentricity errors, an algorithm compensation method based on a calibration experiment using a single reading head was proposed to realize a low-cost and high accuracy angular position measurement. Moreover, the traditional hardware compensation method using double reading heads was also developed for comparison. Firstly, the single gimbal control moment gyroscope system of satellites was introduced. Then, the errors caused by the installation of the reading head were studied and the mathematic models of these errors were developed. In order to construct the compensation function, a calibration experiment using the autocollimator and 24-sided prism was performed. Comparison of angle error compensation using the algorithm and hardware method was presented, and results showed that the algorithm compensation method proposed by this paper achieved the same accuracy level as the hardware method. Finally, the proposed method was further verified through a control system simulation.
机译:圆形光栅的精度是民用微敏捷卫星中使用的单云台控制力矩陀螺仪伺服系统控制精度的关键。代替使用多个读数头消除偏心误差,提出了一种基于校准实验的算法,该算法使用单个读数头来实现低成本和高精度的角位置测量。此外,还开发了使用双读取头的传统硬件补偿方法进行比较。首先介绍了卫星单云台控制力矩陀螺仪系统。然后,研究由读数头的安装引起的误差,并建立了这些误差的数学模型。为了构建补偿功能,使用自动准直仪和24面棱镜进行了校准实验。通过算法和硬件方法对角度误差补偿进行了比较,结果表明本文提出的算法补偿方法达到了与硬件方法相同的精度水平。最后,通过控制系统仿真进一步验证了该方法的有效性。

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