Description: ：查看GPS的卫星个数和状态。 路径分析：屏幕选取起止点、文字录入起止点、 最短路径分析、最优路径分析轨迹回放：导航轨迹播放（ ... iDD (位vb MapX程序-: View the number of GPS satellites and the state. Path Analysis : screen selected starting and ending points, text input starting and ending point, the shortest path analysis, the optimal path trajectory analysis intervals : navigation track player (... iDD (vb - MapX procedures Platform: |
Size: 8855 |
Author:朱雨 |
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Description: ：查看GPS的卫星个数和状态。 路径分析：屏幕选取起止点、文字录入起止点、 最短路径分析、最优路径分析轨迹回放：导航轨迹播放（ ... iDD (位vb MapX程序-: View the number of GPS satellites and the state. Path Analysis : screen selected starting and ending points, text input starting and ending point, the shortest path analysis, the optimal path trajectory analysis intervals : navigation track player (... iDD (vb- MapX procedures Platform: |
Size: 8192 |
Author:朱雨 |
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Description: 根据导弹仿真数据，绘制可直观显示弹道特性的理想弹道曲线。给出了比例导引法的差分方程，建立了
比例导引法的三维弹道仿真模型。在对比例导引法进行三维弹道仿真的基础上，分别对增量比例导引、基于二次
型的最优制导律和考虑动态特性的二次型最优制导律进行了三维弹道仿真，绘制出了可直观显示弹道特性的理想
弹道，计算了导弹与目标的遭遇时间，并对结果进行了比较分析。最后得出考虑弹体动态特性的二次型最优制导
律具有最优性。-According to the missile simulation data, mapping can be visual display characteristics of an ideal ballistic ballistic curve. Proportional navigation law gives the differential equation, proportional navigation law established a three-dimensional trajectory simulation model. Proportional navigation in the three-dimensional trajectory simulation method, based on the respective proportion of the incremental guidance, based on quadratic optimal guidance law and consider the dynamic characteristics of quadratic optimal guidance law for a three-dimensional trajectory simulation, rendering a visual display may be the ideal ballistic trajectory characteristics, calculated the missile with the target Platform: |
Size: 189440 |
Author:特步 |
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Description: 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x的最优函数值；
％-Start a free client and terminal dynamic programming, and the reverse indicator function of the minimum calculation algorithm recursive. x is the state variable, a state on behalf of a stage M-function DecisFun (k, x) by the phase k of state variable x obtained the permission of the corresponding decision variable M-function ObjFun (k, x, u) is the phase indicator function, M-function TransFun (k, x, u) is the state transition function, x is the phase in which a k state variables, u is the corresponding decision variable output p_opt from 4 poses, p_opt = [serial number of group Optimal Strategy Group Group optimal trajectory indicator function value group] fval is a column vector, each element of the, respectively, the optimal strategy p_opt group before the end of the corresponding optimal state function x Platform: |
Size: 2048 |
Author:haiyan |
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Description: 针对助推- 滑翔导弹的弹道优化问题,给出了一种求解其最大射程弹道的分段优化方法,建立了其
纵平面运动模型和弹道优化模型。在考虑攻角绝对值、攻角变化率、法向过载、分离点攻角衔接及落地条件等约束
下,应用序列二次规划法求解了其最大射程弹道。分析表明,助推- 滑翔导弹比传统弹道导弹射程显著提高,其最
优弹道的起伏有助于增大射程和提高突防能力-For booster- Optimize glider ballistic missile problem, give a maximum range of its ballistic solution of the sub-optimization method, set up the vertical plane motion model and optimization model of trajectory. In considering the absolute angle of attack, the rate of change of angle of attack, normal load, the separation point of convergence and the arrival angle of attack constraint conditions, the application of sequential quadratic programming method to solve a maximum range of its ballistic. Analysis showed that propelled- gliding range ballistic missile than the traditional significantly improve, the optimal trajectory of the ups and downs will help increase the range and ability to enhance penetration Platform: |
Size: 381952 |
Author:王敏 |
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Description: SIAM s Advances in Design and Control series consists of texts and monographs dealing with all
areas of design and control and their applications. Topics of interest include shape optimization,
multidisciplinary design, trajectory optimization, feedback, and optimal control. The series focuses
on the mathematical and computational aspects of engineering design and control that are usable
in a wide variety of scientific and engineering disciplines. Platform: |
Size: 18018304 |
Author:simon |
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Description: 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 description of the process, the cost to be minimised, subject to equality and inequality
constraints, using orthogonal collocation on fi nite elements method. Platform: |
Size: 766976 |
Author:陈旭 |
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Description: 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 Platform: |
Size: 1024 |
Author:alicethe |
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Description: 针对登月舱上升段轨迹优化问题，建立上升舱动力学模型，用无量纲技术建立最优控制模型；以燃料消耗最优为指标，利用Pontrjagin极小值原理，将问题转化为时间自由的两点边值问题(TPBVP)。采用一种基于初值猜测方法和向前扫描法求解TPBVP，得到最优上升轨迹。仿真结果表明：此方法收敛速度快、可靠性高，为月面返回实际应用提供一定的参考。-According to the problem of trajectory optimization for the lunar module in ascent stage, firstly, the dynamical model of the module is established, as well as the non-dimensional optimal control-oriented model, secondly, to realize the minimal fuel consumption, the optimal problem is converted into a time free Two-Point Boundary Value Problem (TPBVP) based on the Pontrjagin’s minimal principle, finally, TPBVP is solved and the optimal trajectory is obtained using an initial value hypothesizing method along with the Forward Sweep Algorithm. The simulation results show that this method has advantages of rapid convergence velocity and high reliability, and can provide reference for the practical application of the module returning from moon Platform: |
Size: 357376 |
Author:chenshan |
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Description: 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x的最优函数值； -The beginning and end of the free dynamic programming, find the minimum index function recursive algorithm for computing the reverse procedure. x is the state variable, a represents a phase state M-function DecisFun (k, x) from the stage of the state variable x k of the corresponding enable decision variables determined M-function ObjFun (k, x, u) is the phase index function , M-function TransFun (k, x, u) is the state transition function, where x is the phase of a state variable k, u is the corresponding decision variables output p_opt constituted by a 4, p_opt = [NO group optimal strategy group optimal trajectory group indicator function value group] fval is a column vector, each element represent p_opt optimal strategy group corresponds to the beginning of each end state x optimal function value Platform: |
Size: 2048 |
Author:mengxi |
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Description: matlab 代码，主要用于抛光轨迹的优化，计算个点磨粒的经过次数-matlab code, mainly used for polishing the optimal trajectory, after calculating the number of abrasive points Platform: |
Size: 1024 |
Author:易度 |
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Description: 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.) Platform: |
Size: 2048 |
Author:smile2816
|
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Description: 在给定系统二阶模型、初值、终值、边界约束和路径约束、目标函数的情况下，该程序可利用hp-自使用伪谱法解算出系统从初值到终值的最优轨迹。(Given the second-order model, initial value, final value, boundary constraint and path constraint, and objective function of the system, the program can use hp-self pseudo-spectral method to calculate the optimal trajectory of the system from the initial value to the final value.) Platform: |
Size: 3072 |
Author:桓师 |
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Description: Studied RL agent-based Guidance Laws and Optimal Control techniques for Surface-to-Air Missile Guidance
- Simulated optimal trajectory for the surface to air ballistic missile by implementing Gradient method as an optimization technique in MATLAB Platform: |
Size: 149899 |
Author:legendofseeker |
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Search - optimal trajectory