1) in-phase state
同相状态，等相状态
3) Adjacent state
相邻状态
1.
By simulated annealing method,this paper provides a principal for determining perfect adjacent state.
针对具体实例，给出了相邻状态、迭代长度以及各阶段温度的确定原则。
2.
Akind of function is to produce adjacent states.
针对一类非线性规划问题 ,将模拟退火算法进行了改进 ,提出了一种相邻状态的产生函数 ,为研究非线性规划提供了新的有效求解途径。
3.
According to the property of the continuous variable prob-lem,a function of producing adjacent state is proposed ,and effects of initial temperature,terminal temperatnre as well as annealing schedule to the opti-mal calcuation are analysed,and their suitable scopes are given.
文中根据连续变量问题的特性，提出了一种相邻状态的产生函数和迭代方案，并分析了模拟退火过程的起始温度、终止温度以及降温速度等参数对优化计算的影响，给出了这些参数的适宜区域，通过三个例题的计算，将模拟退火法与传统优化方法一梯度法进行了对比分析，结果表明该法能够有效地解决传统的确定型优化方法所不能奏效的全局优化问题。
4) state-dependent
状态相关
1.
Based on a set of stress path tests,numerical simulation of the deformation behavior of saturated sand in triaxial consolidation and drained tests under different stress paths was carried out by use of the state-dependent sand model.
在一组应力路径试验的基础上,利用砂土的状态相关本构模型,对不同应力路径下饱和砂土在三轴固结排水剪切过程中的变形特性进行模拟。
2.
The so called state-dependent dilatancy theory .
近来一些学者纷纷将土的密度作为变量引入剪胀方程,提出了状态相关剪胀理论,成功地模拟了砂土的各种变形特性。
3.
A state-dependent sand model is implemented in a fully-coupling finite element program to investigate the strain localization problems in sand under drained plane strain condition.
一种状态相关本构模型被置于耦合的有限元程序中,分析了平面应变条件下饱和砂土在排水剪切过程中的变形局部化问题。
5) state-dependent
状态相依
1.
An M/Ej/1 multiple vacation queue system with balking and state-dependent service rate is studied.
研究了带有止步和状态相依服务率的M/Ej/1多重休假排队系统,主要在多重休假排队系统中增加了止步和状态相依两个因素。
2.
A M/Hk/1 queuing system with balking and state-dependent service was studied in this paper.
本文研究了带有止步和状态相依的M/Hk/1排队系统,建立了排队模型的拟生灭过程并获得了系统的平衡条件。
6) relative state
相对状态
1.
Aiming at the problem of improving spacecraft~′s relative state parameters measure precision,the error factors of spacecraft relative state measure technique based on monocular computer vision and target feature are analyzed.
针对提高航天器间相对状态参数测量精度问题,分析了基于单目计算机视觉及目标特征的航天器间相对状态测量方法的误差因素。
2.
According to the project using wireless and laser methods to measure the relative state of two spacecrafts, measuring model was built.
根据所提出的利用无线电和激光测量两航天器相对状态的测量方案,利用动力学法建立了关于待估参数即两航天器相对位置参数的动态状态方程,建立了测量方程,利用卡尔曼滤波法对相对位置进行解算,分析了克服滤波发散的方法,给出了具体仿真算例,通过对仿真结果的分析发现,提出的模型与解算方法可有效提高航天器间的定位精度。
3.
According to the imaging theory of the image sensor, the relative states between objective spacecraft and image sensor are calculated by using the spatial coordinates in object frames of feature-points with symmetry structure and their coordinates in image plane frames.
该方法利用具有对称结构的目标特征点在物体坐标系中的空间坐标以及它们在像平面坐标系中的图像坐标,根据透视成像理论,解算出目标航天器与图像传感器的相对状态。
补充资料：相等
1.犹相同。 2.等待。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条