搜索资源列表
aerolab1.3
- 一款十分实用的可绘制导弹气动外形的工作软件，画图迅速，精确，十分难得！-A wonderful software for drawing many missile configurations!
coe_gui
- 空空导弹设计，可以全面的介绍，分析空空导弹的一般控制和分析流程-Air-to-air missile designed to introduce a comprehensive analysis of air-to-air missile control and analysis of the general process
LabVIEW-basedsimulationoftheopenspacesystemdesignb
- 基于LabVIEW的空地导弹弹道仿真系统设计-LabVIEW-based simulation of the open space system design ballistic missile
danyijianmo
- ANSYS弹翼建模方法及其源代码，详细描述了ANSYS建模过程，针对给定导弹参数建立了导弹弹翼模型并对其进行应力应变分析。-ANSYS wing modeling method and its source code, a detailed descr iption of the ANSYS modeling process, parameters for a given missile missile wing was established models and analysis of st
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
missle--control--design
- 导弹控制系统鲁棒设计程序源代码，可以用来参考编程，比较实用-missile control system design
bili
- 平行接近法弹道仿真。比例导航法，亦称比例导引法，是指导弹飞行过程中速度矢量 的转动角速度与目标视线的转动角速度成比例的一种导引方法。通过建模仿真，使大家更形象生动的理解平行接近法。-Parallel close to the law trajectory simulation. Proportional navigation law, also known as proportional navigation law the missile flight velocity vector rota
qianzhiliangfa
- 前置量法弹道仿真。前置量法也称角度法或矫直法，采用这种导引方法导引导弹时，在整个飞行过程中，导弹-制导站的连线始终提前于目标-制导站连线，而两条连线之间的夹角 则按某种规律变化。通过建模仿真，使大家更形象生动的理解前置量法。-Front method of trajectory simulation. Front Method, also known as the angle law or straightening method, using this guide guided missile
sandianfa
- 三点法弹道仿真。三点法导引是指导弹在攻击目标过程中始终位于目标和制导站的连线上的一种导引方法。通过建模仿真，使大家更形象生动的理解三点法。-Trajectory Simulation of the three-point method. The three-point method guide refers to the guided missile targets is always in the process of a guide on the objectives and guidanc
Anti-ARM
- 介绍当前有关对抗反辐射导弹（ARM）的英文文献，有一定参考价值-Introduction to the fight against anti-radiation missile (ARM) English literature, has certain reference value
Glide-trajectory-calculation
- 一种的滑翔导弹弹 道 的算法C程序-A C-based glide missile trajectory algorithm
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.