Skin-electrode impedance balance was approached through a circuit for automatic matching and gradual approximation optimization algorithm.
这种方法通过设计皮肤电极阻抗自动补偿电路和逐次逼近优化算法实现皮肤电极阻抗自动平衡。
Approximation management framework is a model management framework that based on trust region method, and it aims to construct an optimization method that based on different models.
变可信度模型管理结构是在信赖域方法的基础上，为建立基于不同分析模型的优化方法提出的模型管理框架。
Optimization techniques are being applied to solve the problems of surface interpolation, approximation, smooth joining and fairing, aiming at corresponding goal functions.
只要选用相应的目标函数，曲面插值、逼近、拼接和光顺都可以使用优化技术统一处理。
To improve the method, we make use of indirect approximation method to solve the optimization problem.
为了改进所给出的方法，用间接逼近方法求解优化问题。
A quasi analytic method for solving structural optimization problems is developed by coordinated use of mathematical transformations, high quality approximation and two level approximation strategy.
协同利用数学变换、高精度近似和二级逼近策略，提出了一种求解结构优化问题的准解析法。
The result shows that the optimization method based on approximation technology has good global performance and also can greatly save the calculating resources.
结果表明基于近似模型的优化方法不仅全局性良好，而且有效节约了计算资源。
An efficient solution method for structural optimization is proposed by coordinated use of mathematical transformation, two level approximation concepts and dual theory.
利用包络函数、二级近似概念和对偶理论，提出了一种结构优化的有效解法。
For aerodynamic shape optimization, the approximation management framework (AMF) method was used to organize and manage the variable-fidelity models.
在气动外形优化中，采用近似模型管理结构(amf)方法，对变可信度模型进行组织和管理。
The response surface approximation models are used to replace the original complex vehicle performance model, the optimization is conducted using a sequential quadratic programming algorithm.
通过响应面近似模型的优化，完成了高超声速巡航飞行器的多学科设计优化。
A new approximation method for dealing with stress constraints in structural optimization is presented.
提出一种处理结构优化应力约束的新近似方法。
In addition, the flight path optimization algorithm based on energy state approximation is summarized.
而且，总结了基于能量状态近似法的飞行轨迹优化算法。
This paper presents a sequential approximation method specifically for engineering optimization problems with the three characteristics.
本文提出了一种连续的近似方法，专门为工程优化问题的三个特点。
The approximation of the primal quadratic optimization model can be obtained by solving the regularized one and adjusting the homotopy parameter.
然后通过调节同伦参数，对每个不同的参数用复制子等式进行求解，从而得到原二次规划模型近似解。
By the simulation of a sample path, and the approximation to performance potentials via neural networks based on reinforcement learning (RL), the systems optimization methods are provided.
在样本轨道仿真的基础上，利用神经网络进行强化学习仿真逼近系统的性能势，进而对系统进行优化。
This paper presents a new polygonal approximation approach based on the particle swarm optimization (PSO) algorithm.
本文提出一种新的基于多边形逼近算法的粒子群优化算法。
Then by utilizing the features of this model an online optimization algorithm that combines policy gradient estimation and stochastic approximation is derived.
然后利用这种模式的特点，在线优化算法相结合的策略梯度估计及随机逼近而得。
An approximation algorithm was given to find an out-branching with many leaves in the reduced digraph. Furthermore, some optimization rules were given to improve the out-branching.
对于用近似算法求得的出分枝，又结合前面的规约规则设计了优化规则，以进一步通过优化变换增加出分枝的叶子节点。
To increase the efficiency of the multidisciplinary optimization of aircraft, an aerodynamic approximation model is improved.
在比值修正模型所构造的气动近似模型的基础上，引入了基于实例的推理技术对其加以改进。
The sequential outer approximation approach can give a global optimization solution to the original problem.
该非线性优化问题用渐进外逼近算法可求出其全局最优解。
The sequential outer approximation approach can give a global optimization solution to the original problem.
该非线性优化问题用渐进外逼近算法可求出其全局最优解。
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