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首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers >Identification of the time-varying modal parameters of a spacecraft with flexible appendages using a recursive predictor-based subspace identification algorithm
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Identification of the time-varying modal parameters of a spacecraft with flexible appendages using a recursive predictor-based subspace identification algorithm

机译:使用基于递归预测子的子空间识别算法识别带有柔性附件的航天器的时变模态参数

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This study focuses on the recursive identification of the time-varying modal parameters of on-orbit spacecraft caused by structural configuration changes. For this purpose, an algorithm called recursive predictor-based subspace identification is applied as an alternative method to improve the computational efficiency and noise robustness, and to implement an online identification of system parameters. In the existing time-domain identification methods, the eigensystem realization algorithm and subspace identification methods are usually applied to obtain the on-orbit spacecraft modal parameters. However, these approaches are designed based on a time-invariant system and singular value decomposition, which require a significant amount of computational time. Thus, these methods are difficult to employ for online identification. According to the adaptive filter theory, the recursive predictor-based subspace identification algorithm can not only avoid the singular value decomposition computation but also provide unbiased estimates in a general noisy framework using the recursive least squares approach. Furthermore, in comparison with the classical projection approximation subspace tracking series recursive algorithm, the recursive predictor-based subspace identification method is more suitable for systems with strong noise disturbances. By establishing the dynamics model of a large rigid-flexible coupling spacecraft, three cases of on-orbit modal parameter variation with time are investigated, and the corresponding system frequencies are identified using the recursive predictor-based subspace identification, projection approximation subspace tracking, and singular value decomposition methods. The results demonstrate that the recursive predictor-based subspace identification algorithm can be used to effectively perform an online parameter identification, and the corresponding computational efficiency and noise robustness are better than those of the singular value decomposition and projection approximation subspace tracking series approaches, respectively. Finally, the applicability of this method is also verified through a numerical simulation.
机译:这项研究的重点是递归识别结构结构变化引起的在轨航天器的时变模态参数。为此,一种称为基于递归预测子的子空间识别的算法被用作替代方法,以提高计算效率和噪声鲁棒性,并实现系统参数的在线识别。在现有的时域识别方法中,通常采用本征系统实现算法和子空间识别方法来获得在轨航天器的模态参数。但是,这些方法是基于时不变系统和奇异值分解而设计的,这需要大量的计算时间。因此,这些方法难以用于在线识别。根据自适应滤波器理论,基于递归预测器的子空间识别算法不仅可以避免奇异值分解计算,而且可以使用递归最小二乘法在一般的噪声框架中提供无偏估计。此外,与经典的投影近似子空间跟踪系列递归算法相比,基于递归预测子的子空间识别方法更适合于噪声干扰较大的系统。通过建立大型刚柔耦合航天器的动力学模型,研究了三种情况下在轨模态参数随时间变化的情况,并使用基于递归预测子的子空间识别,投影逼近子空间跟踪和奇异值分解方法。结果表明,基于递归预测器的子空间识别算法可以有效地进行在线参数识别,其计算效率和噪声鲁棒性分别优于奇异值分解和投影近似子空间跟踪序列方法。最后,还通过数值模拟验证了该方法的适用性。

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