搜索资源列表
missilesimulation
- 导弹拦截的仿真程序，用Matlab实现。-missile interception simulation program, using Matlab.
6DOF
- 导弹六自由度仿真模型,并且仿真了导弹攻击一个匀速直线运动的目标的过程-missile six degree-of-freedom simulation model and simulation of a missile attack on a uniform linear motion of the target
six_dof_property
- 导弹的fluent动网格的动态变化源文件代码-Missile dynamics fluent moving mesh source code
SINS-CNS.rar
- 弹道导弹SINS/CNS组合导航的程序，在发射点惯性坐标系下,Ballistic Missile SINS/CNS Integrated Navigation of the program, the launch point inertial coordinate system
STTpd
- STT导弹六自由度仿真，全弹道仿真，侧滑转弯-STT missile 6-DOF simulation
WSP
- 导弹轨道仿真源代码，模型可见钱杏芳《导弹飞行学》第二章的建模，采用四阶龙哥库塔仿真-Missile trajectory simulation source code, the model can be seen Qian Xing-fang, " Missile Flight Science," Chapter II of the modeling, simulation of a four-order Longge Kuta
simulink
- 我这有几篇文章，是关于导弹建模的，主要适用simulink建模并仿真，希望对大家有所帮助。-I have several articles, on the missile model, the main application of simulink modeling and simulation, we hope to be helpful.
BTT
- BTT导弹六自由度仿真，全弹道仿真，倾斜转弯-BTT missile 6-DOF simulation
v1_turbine
- ANSYS的导弹尾翼建模及其气动分析， 是卡耐基梅隆大学网站上的一个ANSYS气动分析应用的例子，帮助理解ANSYS建模与分析，非常经典。-ANSYS modeling and aerodynamic missile fin analysis, is a Carnegie Mellon University on the website an example of application of ANSYS aerodynamic analysis to help understand the
Kepler_orbit_rotate
- 计算得出导弹的被动段飞行轨迹（未考虑大气）和再入点、落点信息（在发射惯性坐标系内的位置量）-Calculated the passive missile flight path segment (not to consider the atmosphere) and re-entry point, placement of information (in the firing position within the inertial coordinate system volume)
bili
- 导弹飞行过程中采用比例导引法，本程序对飞行轨迹就行模拟计算。-Missile flight in the proportional guidance law, the procedures of the flight path on-line simulation.
Advanced-Missile-Guidance-Law-of-the-best-in-the.r
- 先进空空导弹最优中制导律研究Advanced Missile Guidance Law of the best in the-Advanced Missile Guidance Law of the best in the
missile-dynamic
- 根据导弹相对动力学方程用m文件和simulink进行仿真计算-According to the missile with relative dynamics equation m file and simulink for simulation calculation
Missile-Fly
- 导弹飞行轨迹的数值模拟程序（已知初始位置及状态），考虑了科氏力和地球自转的影响，比较实用。-Numerical simulation of the missile trajectory program (known initial position and status), taking into account the Coriolis force and the Earth s rotation, more practical.
Missile-Trajectory-Simulation
- 导弹弹道仿真 通用导弹、炮弹、火箭弹等的弹道仿真计算程序，适用于无控*，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。-Missile Trajectory Simulation
missile-proportional-navigation
- 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
simulation-of-missile
- 导弹在通过气动力控制几种匀速直线运动目标的simulink文件-Six degree of freedom simulation of missile
missile
- 导弹仿真，比较清楚，适合初学者。matlab仿真-missile simulation
Air-defense-missile
- 对防空导弹的拦截弹道进行了仿真了，主要特点是采用了模块化设计。-The airlift missile intercepted trajectory was simulated, the main feature is the use of modular design.
PDF+simulink
- 针对某些导弹在对目标进行打击时需要满足零脱靶量和攻击角度约束的要求,首先基于终端滑模控制和有限时间控制理论,改进了一种快速收敛的非奇异终端滑模函数,用于设计滑模面,结合自适应指数趋近律,提出了一种自适应非奇异终端滑模控制方法。(For some missile needs to meet the zero miss distance and attack angle constraint requirements in the attack on the target, based on the