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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
vertex
- 该程序可用于计算无后缘后掠角的平板梯形翼在小攻角时升力与升力系数-This program can be used to calculate the plate without posterior trapezoidal wing sweep angle of attack in the small lift and lift coefficient
cxcy
- 黑鹰桨叶升力/阻力/力矩系数随迎角变化数据模型-The paddle lift/drag/moment coefficient different angles of attack data
GPNattackzone
- 中程空空导弹火控系统广义比例导引攻击区绘制程序（vs2012编译平台下编写）-Attack zone under the generalized proportional guidance law(programmed in visual studio 2012)
Shock-Wave-Calculation
- 用CFD方法计算超声速下小攻角翼型产生的激波-CFD method with a small angle of attack under supersonic shock wave generated airfoil
fangzheng0
- 该程序是对飞行器的航迹进行模拟。包括3个文件，主程序是fangzhen.m，可以反映出飞行器高度、速度、攻角等参数对飞行器航迹的有效-The program is a simulated aircraft track. Includes three files, the main program is fangzhen.m, can reflect the aircraft altitude, speed, angle of attack of the aircraft trajectory p
angleOfg2b
- 基于simulink建立了飞机六自由度模型，并计算其迎角。-Based on simulink established six degrees of freedom model aircraft, and calculate the angle of attack.
Fluent-history-result-postprocess
- Fluent软件通常用于航空航天领域，本程序可以实现对Fluent计算结果的自动提取，并且按照来流迎角对升阻力、力矩系数排序，最后生成结果文件-Fluent software is typically used for aerospace applications, this program can achieve automatic extraction Fluent calculation results, and in accordance to the flow angle of att
ATTDesign
- 用于设计外形，得出合适的空泡形状，同时可变攻角，的书理论空泡外形-Theory in shape for the cavity design shape, draw a suitable cavity shape while variable angle of attack, the
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
一种带落角约束的精确制导律（拦截高超声速目标）
- 一种考虑终端攻击角度约束、拦截高超声速目标的精确制导方法仿真(Simulation of an accurate guidance method considering terminal attack angle constraint and intercepting hypersonic target)