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- The root loci analysis of the gyroscopic mechanical structural system controlled by a damper is presented. 对受粘性阻尼器控制的机械结构系统进行了根轨迹分析，着重研究了根轨迹分岔现象。
- root locus analysis [计] 根轨迹分析
- Root Loci Analysis of Gyroscopic System with a Viscous Damper 具有粘性阻尼器的陀螺系统根轨迹特性分析
- Classical controls approach to the analysis and design of digital control systems.Design by frequency response and root locus methods. 以离散时间的观念来分析系统，建立模式及达成控制器设计，并探讨其实际应用上的问题。
- A new expression of root locus equations is derived. 导出一种根轨迹代数方程的新表达式。
- INFLUENCE OF DAMPER ON THE EIGENVALUES OF MECHANICAL STRUCTURAL SYSTEM USING ROOT LOCI ANALYSIS 应用根轨迹分析阻尼器对机械结构系统特征值的影响
- The analyses on the variable centroid controlled spinning missile were made by utilizing the root locus method. 摘要利用根轨法对变质心控制旋转导弹的稳定性进行分析，给出了变质心控制导弹稳定的充分必要条件。
- Based on the root locus properties, small desired closed-loop time constant may result in ringing in the presence of plant model mismatches. 根据根轨迹的性质，当存在模型失配时，较小的期望闭环时间常数将导致控制器的输出产生振铃现象。
- The dynamic stability is studied for load factors ranging from 1 to 4 . The charactristics of mode of motion are identified and analysed by root locus plots and Argand diagrams. 研究了过载因子n_y从1到4时对该机运动稳定性的影响,用根轨迹图和表示特征向量的阿冈德(Argand)图识别和分析了各运动模态的特性。
- A comparison result of the stability of the control system is given by the Root Locus and Nyquist stability criterion while with or without inserting the compensation loop. 通过对太阳望远镜在吊篮中运动的控制模型的分析，指出了控制回路的高级补偿设计是望远镜克服吊篮在水平面内摆动的影响而实现高精度指向控制的关键因素之一。
- THE ANALYSIS OF NON-LINER OSC ILLATION BY USING ROOT LOCUS METHOD 用根轨迹法分析非线性自激振荡器
- Another very useful graphical technique deals directly with the roots of the characteristic equation. This second method is called the root locus method. 而另一种很有用的图解法研究特征方程的根，这种方法称为根轨迹法。
- On teaching variable multi-parameter root locus 多参变量根轨迹教学初探
- Special problem of parameter root locus 参数根轨迹中的特殊问题
- Improving Discussion of Root Locus 根轨迹仿真的改进探讨
- A Computational Technique for the Robust Root Locus 根轨迹推演
- The taxpayer do not have locus stand in this court. 该纳税人没有在法庭上的陈述权。
- Classical linear flutter analysis is based on the solution of flutter eigenvalue problem, and needs to track the root loci to determine the correct flutter boundary but sometimes it may fail. 摘要经典的线性颤振分析方法需要求解颤振特征值问题，并需要对特征值进行跟踪排序，以消除在确定颤振临界点时可能出现的颤振模态分支的“窜支”问题，从而影响了颤振分析的效率及自动化程度。
- Computer Aided Design of Lag- lead Compensator Based on Root Locus 基于根轨迹法的滞后-超前补偿器的计算机辅助设计
- Design of Lag Compensator Based on Root Locus in MATLAB Environment MATLAB环境下基于根轨迹法设计迟后补偿器
