The parameter plane is divided into stable region and self-oscillating region.
将参数平面划分为稳定区和自振区。
The bifurcation diagrams of the parameter plane and the response equation are obtained.
给出主参数共振系统参数平面的分岔集和幅频响应方程的分岔图。
The stabilities of the equilibrium points and limit cycles in different regions of two parameter plane are studied.
在两个参数平面上研究了系统在余维二分叉点附近的不同区域内平衡点和极限环的稳定性及其个数。
If only the phase fluctuation is included in the incident light, the correlation time can also affect the parameter plane of the FOLT.
当入射光仅包含位相涨落时，噪声相关时间对一级相变类比的参数区域也产生很大影响。
The fuzzy logic was used to describe 3 contours of fuzzy membership on parameter plane. Also fuzzy membership of various cardiovascular statuses could be achieved.
利用模糊数学等方法得到3幅参数平面上的隶属度等势线图，并确定心血管状态的二维隶属度。
The above two indexes were utilized to establish a parameter plane. The plane was divided into 9 areas to indicate various cardiovascular statuses by 'Youden index'.
用外周血管评估指数和心功能评估指数构成参数平面，应用约登指数将该平面分割为9个区域，分别对应不同的心血管状态；
Using the analytical relationship, many boundaries namely scissors sketed, could be drawn on the parameter plane of horizontal tail area and aeroplane center of gravity.
利用这种解析关系，可以在平尾相对面积和飞机重心位置的参数平面上，绘制出各种限制边界，形成所谓“剪刀图”。
Based on the averaged equation, the transition boundaries are sought to divide the parameter plane into different regions, corresponding to different types of the solutions.
基于平均方程，得到了参数平面上的转迁集，这些转迁集将参数平面划分为不同的区域，在各个不同的区域对应于系统不同的解。
In this paper a new parameter plane method is proposed and is used to design the stability augmentation control system of a certain type of aircraft and satisfactory results are obtained.
本文提出了一种新的参数平面法，设计了某型歼击机的控制增稳系统，并取得了满意的结果。
In this paper a new parameter plane method is proposed and is used to design the stability augmentation control system of a certain type of aircraft and satisfactory results are obtained.
本文提出了一种新的参数平面法，设计了某型歼击机的控制增稳系统，并取得了满意的结果。
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