maximum principle

Maximum principle of semi-linear distributed system(ⅰ)

半线性分布系统的最大原理（Ⅰ）

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We establish the Pontryagin's maximum principle for the time optimal control problem governed by the 2-dimensional Boussinesq system as well.

对2维Boussinesq方程时间最优控制问题给出了最大值原理。

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The maximum principle of slope difference for the extraction of feature points of the weld& stripe axis is presented. A strict proof for the unbias statistics of the principle is offered.

提出了焊缝光纹中轴特征点提取的极大斜率差原理，并对其无偏特性给出了严格的证明。

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At the end of the article, a control code is derived with the maximum principle.

然后利用极大值原理导出了控制律。

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By Pontriaghin Maximum Principle, necessary condition and boundary condition of optimal trajectory were obtained.

通过极大值原理推导出时间最短弹道优化问题的必要条件和边值条件。

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A dynamic corporate firm model was developed for differential games, with the Maximum Principle of Pontryagin combined with the path coupling procedure of van Loon to analyze the coordinating and adapting processes of the firms in games.

借鉴微分对策的思想，结合最优控制理论中Pon-tryagin极大值原理和Van Loon路径耦合方法，研究了两家股份制企业之间不断协调和相互适应的博弈过程；

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In this paper the time optimal control problem for nonlinear integral control systems with weak singularity kernel is discussed, and it is proved that the Pontryagin maximum principle is still applicable to this system.

本文讨论具弱奇性核的非线性积分系统的快速控制问题，证明了最大原理对这种系统依然适用。

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Analysis of short-term power system disturbance Based-on modulo maximum principle and energy distribution curve of wavelet transform

基于小波变换模极大值原理和能量分布曲线的电力系统短期扰动分析

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A Maximum Principle for Stochastic Optimal Impulse Control

随机系统最优脉冲控制的最大值原理

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The paper changes the non-linear equation into a non-linear parabolic equation by a kind of change and proves the blow up of solution of its initial boundary value problem in finite time by using convexity method and maximum principle.

本文以一种变换。化非线性方程为非线性抛物型方程，并利用凸性方法及最大值原理证明其初边值问题的解于有限时间内blow up。

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the cauchy-dirichlet problem for a degenerate equation in two sides: uniqueness and maximum principle of weak solution

一类双边退缩的抛物型方程的Cauchy-Dirichlet问题&解的唯一性和极值原理

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this paper is concerned with analysis and study of minimum fuel coplanar transfer with finite thrust by applying pontryagin maximum principle. the solution conditions for optimal trajectories and optimal controls are concerned.

本文从能量最省的角度应用极大值原理对空间飞行器采用有限推力同平面轨道转移的情况进行了分析和研究，得到了最优转移轨道及最优控制的求解条件。

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First, the Maximum principle is used to generate an optimal guidance law for lunar landing, and the TPBVP is to be solved as a result of the numerical solution for optimal trajectory.

文中首先应用极大值原理设计了最优着陆制导控制律，此时求解最优轨迹变成一个两点边值问题（TPBVP）。

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Using separation theorem of convex set and the time terminal value function equation, we obtain the determining method of optimal terminal time as well as the Maximum principle.

由凸集分离定理及终端时间阈值函数方程，我们获得了最大值原理及最优控制时间的确定方法。

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It is shown that the numerical solutions preserve discrete maximum principle.

同时证明了由这2种方法得到的数值解满足离散的最值原理。

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The Regular Embedded Ends and the Maximum Principle at Infinity

正则嵌入端与无穷远极大值原理

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