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[Multimedia program] navigation DL : 0: Zarchan s tacticle and strategic missile guidence
Update : 2008-10-13 Size : 28.03kb Publisher : yixiaoxi
[SCM] extendkalman DL : 0: 卡尔曼滤波器是一个“optimal recursive data processing algorithm（最优化自回归数据处理算法）”。对于解决很大部分的问题，他是最优，效率最高甚至是最有用的。他的广泛应用已经超过30年，包括机器人导航，控制，传感器数据融合甚至在军事方面的雷达系统以及导弹追踪等等。近年来更被应用于计算机图像处理，例如头脸识别，图像分割，图像边缘检测等等。-Kalman filter is an "optimal recursive data proces sing algorithm (since the handover optimization algorithm for data processing). " For most of the solution, he is the best, most efficient, if not the most useful. He has the broad application of more than 30 years, including robot navigation, control, sensor data fusion even in the military aspects of the radar system and missile tracking, and so on. In recent years, it has been used in computer image processing, such as humans recognition, image segmentation, image edge detection, and so on.
Update : 2025-02-17 Size : 1kb Publisher : 于军相
[Other systems] powerview DL : 0: 特种电源装甲车火控系统应用：导弹导航系统 -Special power supply armored vehicle fire control system applications: missile navigation systems
Update : 2025-02-17 Size : 635kb Publisher : mscsoft
[matlab] Missile_Png_Simualtion DL : 0: 本程序包为导弹比例导引仿真计算程序，展现了MATLAB利用MEX接口与Visual C++的完美结合。关键词：导弹弹道比例导引仿真 MEX missile simulation png guidance-The package for the proportion of guided missile simulation procedures, demonstrated MATLAB using MEX interface with Visual C++ Perfect combination. Key words: proportional navigation missile trajectory simulation MEX missile simulation png guidance
Update : 2025-02-17 Size : 14kb Publisher : donotspam
[Multimedia Develop] navigation DL : 0: Zarchan s tacticle and strategic missile guidence -Zarchan s tacticle and strategic missile guidence
Update : 2025-02-17 Size : 28kb Publisher : yixiaoxi
[Software Engineering] rocket DL : 0: 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
Update : 2025-02-17 Size : 185kb Publisher : 特步
[OpenGL program] MISSILETEST DL : 0: 一个导弹的模拟效果，opengl，有例子和导航的效果，-Simulated the effect of a missile, opengl, there are examples and the effectiveness of navigation,
Update : 2025-02-17 Size : 3.55mb Publisher : huachaoluo
[Software Engineering] Matlab_3dof_animation DL : 0: 采用比例导引法,把三维追击轨道分解到两个二维平面上分别导引,并充分考虑到目标的机动性对弹道的影响,用MATLAB软件编写程序模拟出导弹实际追击的三维变轨弹道,绘制出分运动和合运动中各参数的变化曲线。最后比较了不同的追击速度和不同的导引系数k对弹道特性的影响,考虑到导弹实际飞行时受需用法向过载的制约,导出了导引系数k应满足的普遍公式,提出了对实战具有一定参考价值的建议。 -Using proportional navigation law, in pursuit of the three-dimensional orbit decomposition to two two-dimensional plane, respectively, guidance, and taking fully into account the objectives of the impact of mobility on the trajectory, using MATLAB software programming practical pursuit of missile simulated three-dimensional orbit trajectory , to map out points Movement Hop movement curve of each parameter. Finally, the pursuit of different speed and different-guided ballistic coefficient k on the characteristics of, taking into account the actual missile flight by the need to overload the use of constraints derived Seeker coefficient k should satisfy the general formula, put forward on the actual reference value has a certain proposal.
Update : 2025-02-17 Size : 289kb Publisher : 李恒
[matlab] g_r DL : 0: 理想比例导引规律的弹道仿真，用于研究导弹的飞行规律-Proportional navigation trajectory ideal simulation
Update : 2025-02-17 Size : 1kb Publisher : gaochi
[Mathimatics-Numerical algorithms] kalman_intro_chinese DL : 0: 卡尔曼滤波器是一个“optimal recursive data processing algorithm（最优化自回归数据处理算法）”。对于解决很大部分的问题，他是最优，效率最高甚至是最有用的。他的广泛应用已经超过30年，包括机器人导航，控制，传感器数据融合甚至在军事方面的雷达系统以及导弹追踪等等。近年来更被应用于计算机图像处理，例如头脸识别，图像分割，图像边缘检测等等。-Kalman filter is an " optimal recursive data processing algorithm (optimal autoregressive data-processing algorithm)." To address the very most of the questions, he is the best, most efficient, if not the most useful. He has been widely used for more than 30 years, including robot navigation, control, sensor data fusion and even in military radar systems and missile tracking and so on. Recent years been applied to computer image processing, such as头脸recognition, image segmentation, image edge detection and so on.
Update : 2025-02-17 Size : 557kb Publisher : 曲晓川
[ADO-ODBC] dandao DL : 1: 利用比例导引法及龙哥库塔法计算的红旗-2导弹的模拟仿真程序。-Using proportional navigation law and龙哥Kutta method to calculate the red-2 missile simulation procedures.
Update : 2025-02-17 Size : 16kb Publisher : 赌挖宝
[matlab] daodan DL : 0: 比例导引理想弹道仿真Matlab代码，给出了比例导引法的差分方程, 采用Matlab语言, 对比例导引法的导弹理想弹道进行了三维数据仿真, 绘制出三维理想弹道。随导弹与目标参数变化情况, 对理想弹道的特性进行了分析。-Ideal proportional navigation trajectory simulation Matlab code, the law gives the proportional navigation differential equations using Matlab language, the ideal ratio of ballistic missile guidance method for simulation of three-dimensional data, to map out the ideal three-dimensional trajectory
Update : 2025-02-17 Size : 1kb Publisher : madier
[matlab] Proportionalnavigationmethod DL : 0: 用比例导引法进行拦截弹针对机动目标的弹道仿真，仿真是基于三维模型。-Proportional navigation method used to intercept ballistic missile targets for motor simulation, simulation is based on three-dimensional model.
Update : 2025-02-17 Size : 1kb Publisher : 康凯
[Other] Proportional-Navigation DL : 0: 比例导引律，实现在二维平面内导弹拦截目标-Proportional navigation law, to achieve the goal of two-dimensional plane missile interceptors
Update : 2025-02-17 Size : 1kb Publisher : 李磊
[matlab] Missile-algorithm DL : 0: 基于MATLAB导弹仿真源代码(missile simulation) 给出了比例导引法的差分方程, 采用Matlab语言, 对比例导引法的导弹理想弹道进行了三维数据仿真, 绘制出三维理想弹道。随导弹与目标参数变化情况, 对理想弹道的特性进行了分析-Missile simulation based on MATLAB source code (missile simulation) Differential equation gives the proportional navigation law, using Matlab language, ideal ballistic missile proportional navigation law were three-dimensional simulation data and draw a three-dimensional ideal trajectory. With the missile and the target parameters, the characteristics of the ideal trajectory is analyzed
Update : 2025-02-17 Size : 4kb Publisher : 光辉
[transportation applications] Proportional-Navigation--kinematics DL : 0: MATLAB编写的平面比例导引运动学程序，自己写的，可用于导弹导引段过载分析-MATLAB prepared proportion plane kinematics program guide, write your own can be used to guide the missile segment analysis Overload
Update : 2025-02-17 Size : 2kb Publisher : chenfangzheng
[transportation applications] missile-proportional-navigation DL : 1: 导弹以比例导引方式攻击匀速运动目标的三自由度仿真-Three degrees of freedom simulation of missile proportional navigation
Update : 2025-02-17 Size : 16kb Publisher : 陈阳
[Other] Navigation-Trajectory-Simulation DL : 1: 基于MATLAB+GUI的导弹比例导引的三自由度弹道仿真-MATLAB+ GUI based missile proportion of guiding three degrees of freedom trajectory simulation
Update : 2025-02-17 Size : 101kb Publisher : 郑玉玺
[matlab] Missile Guidance DL : 0: missile guidance and navigation using Pagony method
Update : 2025-02-17 Size : 19kb Publisher : alidadgh
[Other systems] Four degree of freedom missile motion equation based on proportional navigation method DL : 2: Four degree of freedom missile motion equation based on proportional navigation method，The motion equation of 4-DOF missile based on proportional guidance method is given, and the termination conditions are given
Update : 2022-10-19 Size : 1.21kb Publisher : 2239538092@qq.com

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