... root locus 根轨迹 root-locus method 根轨迹法 root-mean-square 均平方根的，有效值的，均方根，均方根值 ...
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Using the root locus method, the characteristic equations are analyzed.
利用根轨迹法，分析了特征方程。
Furthermore, it performed the parametric analysis in terms of feedback gains and delayed time using the root locus method, thus obtaining the system's flutter stability boundary.
进而采用根轨迹方法就反馈增益和延迟时间进行参数分析，获得系统的颤振稳定性边界。
A flutter analysis based on root locus method is programmed. It can be applied to a wing equipped with an active flutter suppression system.
本文编制了可用于分析带有颤振主动抑制系统的机翼的根轨迹法程序。
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