搜索资源列表
GA_missile_trajectory_simulation
- 提出了一种空面导弹下滑段、俯冲攻击段的弹道优化设计方案,以及一 种实现航向动态跟踪的具体方法。大量算例表明,采用本文中的空面导弹控制 方案可以设计、调试出较满意的弹道,达到获取导弹飞行性能数据并验证导弹总 体设计参数的目的。 -A decline in air-surface missile paragraph, paragraph ballistic dive attack to optimize the design of programs, as well as a cou
yuanchengfanjiandaodandandaoguihua
- 保证远程反舰导弹迅速捕捉目标为出发点，以远程反舰导弹的作战需求为牵引，论述了对远程反舰导弹进行 弹道规划的重要意义；从战术和技术两个方面探索了对远程反舰导弹进行弹道规划的主要依据、基本原则、规划思路和基本 方法。-To ensure rapid capture long-range anti-ship missile as the starting point goal to long-range anti-ship missiles for the operational requir
the-proportional-guidance--
- 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-Given the proportional guidance law of difference equation, based on Matlab language, for proportional guidance law missile ideal ballistic three-dimensional dat
ballistics problem
- 本程序包为vxLand提供的经典版的通用导弹、炮弹、火箭弹等的弹道仿真计算程序，适用于无控弹药，用户可以需要根据加入三点法、比例导引等导引方法，修改、扩充成相应的有控、制导模拟仿真弹道程序。 -This package provides the classic version of vxLand common missile, artillery shells, rockets and other ballistic simulation program for non-control a
Tomahawk2
- 通过对MatlAB 中Designing a Guidance System in MATLAB® and Simulink® 的导弹质量特性和气动特性的改变，并由原有的3DOF扩展为6DOF，仿真导弹的弹道特性、姿态特性和过载特性。 -In Matlab Designing a Guidance System in the MATLAB ® and Simulink ® missiles quality characteristics and aerodynamic characteris
trajectory
- 用4阶龙格库塔法求解给定攻角情况下的空地导弹弹道。-to solve a given Angle of attack of the ballistic missile with a four order runge kutta method.
standardtrajectory
- 导弹标准弹道计算，可以给出飞行过程中的高度、速度、攻角等信息-Ballistic Missile standards can be given during the flight altitude, speed, angle of attack and other information
zengliangbiliyindao
- 一组有意义的弹道导弹增量比例引导弹道仿真弹道分析程序，分别用一维、二维插值等方法对弹道导弹的弹道进行了仿真，分析了其弹道特性-A set of meaningful ballistic missile incremental proportion guide ballistic trajectory simulation analysis program, with one-dimensional and two-dimensional interpolation method for the
daodandandao
- 导弹三维弹道仿真的MATLAB程序,其中龙格库塔积分的程序很简单且通用性强-Three-dimensional simulation of MATLAB ballistic missile program, which Runge-Kutta integration process is very simple and versatile
r4
- Matlab/simulink 导弹三自由度弹道仿真-Matlab/simulink simulation ballistic missile three degrees of freedom
3dof_MISSILE_SIMULATION_WITH_MATLAB
- 对三自由度的导弹弹道进行了方针分析，并且支持从Simulink中输出弹道数据，两个m文件支持在MATLAB工作界面绘制三维弹道轨迹与生成轨迹TXT文件。-Ballistic missile has carried on the policy analysis of the three degrees of freedom, and support the output of the Simulink ballistic data, two m file support work in MATL
atbm
- 反战术导弹导弹比例导引律三维弹道仿真程序.-The proportion of anti-tactical ballistic missile missile guidance law of three-dimensional trajectory simulation program.
missile_artical
- 系统论述了弹道导 弹的模块化设计思想，并提供了相应的程序-It discussed ballistic missile system of modular design, and provides a corresponding program
CNS
- 弹道导弹SINS/CNS组合导航 Ballistic missile SINS / CNS Integrated Navigation- Ballistic missile SINS/CNS Integrated Navigation
trajectory1
- C语言计算导弹弹道,C语言计算导弹弹道 -C language calculated ballistic missiles, C language calculated ballistic missile
Trajectory-Shape-Varying-Missile-Guidance-for-Int
- Trajectory-Shape-Varying Missile Guidance for Interception of Ballistic Missiles during the Boost Phase
pitch program first stage
- pitch program of ballistic missile first stage
Untitled.zip
- 中程导弹打击轨迹的弹道仿真模拟。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。(Medium-range ballistic missile strikes trajectory simulation)
弹道仿真论文及代码
- 通过各段运动方程模拟弹道导弹飞行过程中各段的导弹轨迹，按照边界条件拼接在一起，实现轨迹的仿真。(The trajectory of each stage in the process of ballistic missile flight is simulated by motion equations, and the trajectory is simulated according to the boundary conditions.)
弹道导弹被动段
- 内附有弹道导弹弹道要求及过程，有完整的matlab程序，可以借鉴学习。自己大三时的远程火箭弹道学大作业。(t includes ballistic missile trajectory requirements and process, complete matlab program, which can be used for reference and learning. My junior year of long-range rocket ballistics homework.)