柔性航天器BCB姿态机动路径的频谱分析与参数选择

Zhen Yu, Chenxing Zhong, Yu Guo
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引用次数: 5

摘要

利用FFT对经典的Bang-Coast-Bang路径谱进行分析,选择适合航天器姿态机动的路径参数。利用DFT方法推导了BCB路径的谱表达式。通过分析BCB路径的频谱特性,研究了路径参数与频谱以及机动时间之间的关系。提出了一种BCB路径参数的选择方法。研究结果表明,采用该方法选择BCB路径参数,可有效降低姿态机动对柔性附件振动的影响,实现快速机动和快速稳定。数值仿真结果验证了该方法的有效性,并为BCB路径参数的选择提供了参考。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Spectral analysis and parameter selection for BCB attitude maneuver path of flexible spacecraft
The classical Bang-Coast-Bang path spectrum was analyzed by FFT in order to select the path parameters which were fit for flexible spacecraft attitude maneuver. Spectrum expression of BCB path was derived by means of DFT. The relation between the path parameters and spectrum as well as maneuver time was studied by analyzing the spectral characteristics of BCB path. A selection method of BCB path parameters was proposed. Research results indicate that if the BCB path parameters are selected by the proposed method, it can effectively reduce flexible appendages' vibration affected by attitude maneuver for rapid maneuver and rapid stabilization. Numerical simulations demonstrate the effectiveness of the method, and it is useful for BCB path parameters selection.
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