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最优制导律反战术弹道导弹TBM弹道仿真,matlab编写。,Optimal Guidance Law TBM anti-tactical ballistic missile trajectory simulation, matlab prepared.
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基于Biegler动态优化正交配置法(联立算法)的matlab 代码,由M.Cizniar,M. Fikar等编写-dynopt is a set of MATLAB functions for determination of optimal control trajectory by
given descr iption of the process, the cost to be minimised, subject to equality and inequality
const
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最优制导律攻击机动目标弹道仿真,matlab编写。-Optimal guidance law for maneuvering target trajectory simulation attacks, matlab prepared.
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自由始端和终端的动态规划,求指标函数最小值的逆序算法递归
% 计算程序。x是状态变量,一列代表一个阶段状态;M-函数
% DecisFun(k,x)由阶段k的状态变量x求出相应的允许决策变量
% M-函数ObjFun(k,x,u)是阶段指标函数,M-函数TransFun(k,x,u)
% 是状态转移函数,其中x是阶段k的某状态变量,u是相应的决策变量;
% 输出p_opt由4列构成,p_opt=[序号组 最优策略组 最优轨线组
% 指标函数值组];fval是一个列向量
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The GUI is used to demonstrate the results and concepts used in the paper.
If readers want to use its result in their research for determining the minimum-length or time-optimal trajectory, just call function
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轨迹优化源代码,用切比雪夫法求解最优控制问题。-trajectory optimal
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LMS算法及仿真实现,在等高线性能平面上绘制出了滤波器系数的运动轨迹和最优滤波器系数,以及错误概率的变化趋势。针对迭代次数变化和迭代步长变换分别作了相关讨论。-LMS algorithm and the simulation realization, in contour performance plane drawing out of the filter coefficient trajectory and optimal filter coefficient, and the change
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自由始端和终端的动态规划,求指标函数最小值的逆序算法递归 计算程序。x是状态变量,一列代表一个阶段状态;M-函数 DecisFun(k,x)由阶段k的状态变量x求出相应的允许决策变量 M-函数ObjFun(k,x,u)是阶段指标函数,M-函数TransFun(k,x,u) 是状态转移函数,其中x是阶段k的某状态变量,u是相应的决策变量; 输出p_opt由4列构成,p_opt=[序号组 最优策略组 最优轨线组 指标函数值组];fval是一个列向量,各元素分别表示p_opt各 最优策略组对应始端状态
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This report considers trajectory planning with constrained dynamics and design of an appropriate
feedforward controller for single axis motion control. A motivation is given for using
model-based fourth order feedforward with fourth order traject
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运用GPOPS求解一个倒立摆问题的优化轨迹,使其能很好保持稳定。(solve trajectory optimal)
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利用GA遗传算法进行动态路径规划,完成最优轨迹的生成,适合新手入门学习。(Using GA genetic algorithm for dynamic path planning, the completion of the optimal trajectory generation, suitable for beginners to learn.)
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基于内点法的最优潮流计算,跟踪中心轨迹内点法最优潮流程序 实现了有功损耗最小的经济分配。(Optimal power flow calculation based on interior point method, the point-of-flight optimal power flow program in the tracking center trajectory achieves the economic distribution with the least active loss
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基于遗传算法的最优时间B样条轨迹,复现文章3.6节中的分析(The time-optimal B-spline trajectory based on genetic algorithm. This programme recurrences the analysis in section 3.6 of this paper)
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