基于系统辨识的X-Y座式卫星天线动力学控制

2019 7th International Conference on Control, Mechatronics and Automation (ICCMA) Pub Date : 2019-11-01 DOI:10.1109/ICCMA46720.2019.8988738

B. Aykent, Kadir Koca, M. Celik

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引用次数: 0

摘要

开发了基于子空间方法的系统辨识方法，并将该方法生成的6种不同的传递函数嵌入到X-Y基座卫星天线的运动控制单元中。这6个传递函数的拟合估计数据在95.46%到99.99%之间变化，RMSE(均方根误差)度在0.00502到0.00984之间，而目标RMSE度值为0.05。

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System Identification-Based Dynamics Control for X-Y Pedestal Satellite Antenna

Subspace method-based system identification and six different transfer functions as product of this method have been developed and embedded in the motion control unit of the X-Y pedestal satellite antenna. Fit estimation data of these six transfer functions is changing from 95.46% to 99.99% with a RMSE (root mean square error) degree from 0.00502 to 0.00984, whereas the target RMSE degree value is 0.05.

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来源期刊

2019 7th International Conference on Control, Mechatronics and Automation (ICCMA)

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