资源列表
ballistic_missile_inertial_navigation
- 弹道导弹从东经120北纬20高度30公里打目标东经150北纬30高度0的目标，关机点及飞行时间计算。还介绍了惯性导航的内容。 对于弹道式导弹：目标作为地球上的某一点，它是随地球一起在惯性空间运动的，因此需要迭代求解需要速度和自由飞行时间。按照给出的程序进行多次迭代解算即可得出考虑地球自转时的关机点参数解算和飞行时间计算。-20 ballistic missile from a high degree of north latitude and 120 east longitude hit tar
satellite_orbit
- 卫星轨道方面的知识，卫星轨道姿态动力学与控制-Knowledge of satellite orbit, the satellite attitude and orbit dynamics and control
bus_search_system
- 公交查询系统 JAVA 做到 实现了 多种查询方案.有 换乘优先,票价优先,路程最短-JAVA query system bus to achieve a variety of query plan to do there transfer priority, the fare first, the shortest distance ...
EEMD
- 求解EEMD的工具箱，里面包含EEMD主程序，可以直接调用-Solving the EEMD toolbox, which contains the EEMD main program, you can directly call it
CFL3D.v6.5
- CFL3D的源代码，Fortran编写，包含求解NS方程，input文件等-the sources of CFL3D ,its Fortran language,contians NS solver,input profiles
openprop.tar
- 升力线模型计算代码，将机翼表征为一个沿展向变化的涡线，通过尾涡计算诱导速度，实现计算的封闭。-Lifting line model code, the characterization of the wing along the exhibition to the change of the vortex line, trailing vortex induced velocity calculated closed.
RCS-computing
- 通过catia建模，并在其中进行网格划分，然后由程序读入，用物理光学法计算其雷达散射截面，该算法经多次使用验证。-Catia modeling, in which mesh is then read by the program, the physical optics method to calculate the radar cross section, the algorithm repeatedly verified.
RCS
- 该语言由matlab实现，通过catia建模，并在其中进行网格划分，然后由程序读入，用物理光学法计算其雷达散射截面，该算法经多次使用验证。-The language by matlab to achieve, by catia modeling, meshing, and then read by the program, physical optics method to calculate the radar cross section, the algorithm repeatedly v
lridex
- matlab函数，专门计算列车车体横向sperling平稳性指标。调用方式：y=lridex(acc)，其中acc为测得的或仿真得到的车体横向加速度（不包括时间列）。-matlab function, specifically calculate the train body lateral sperling smooth indicators. The invocation: y = lridex (ACC), wherein acc obtained for the measured or
VBI-ANSYS
- 采用ansys的位移法和生死单元两种方法实现的车桥耦合程序-The axle coupling procedure using ansys displacement method and life and death are two ways to achieve unit
aircraft-6-DOF-simulation
- 飞行器六自由度建模，以及飞行器配平，线性化的matlab程序-The aircraft six degrees of freedom modeling, as well as aircraft trim, linearization matlab program
flutter-of-plate
- 弹簧支撑二维悬臂板的颤振计算。得到了临界颤振速度，并用图形表示-flutter of plate