资源列表
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
Motor-control
- 发动机matlab模型，可以实现发动机外特性曲线，发动机控制，包括油门开度，转速，转矩等参数-Matlab engine model can be achieved outside the engine characteristic curve, the engine control, including the throttle opening, speed, torque and other parameters
fbyouhua_shijianshangandchidushang
- Morlet小波带宽参数优化，利用shannon小波熵算法，非常实用。里面包括Morlet连续小波变化的实现-Morlet wavelet bandwidth parameters optimized using shannon wavelet entropy algorithm is very practical. Which includes the implementation Morlet continuous wavelet transform
program
- abaqus 二次开发参考资料，包括各种材料子程序UVMAT，加载子程序VDLOAD-abaqus secondary development of reference materials, including a variety of material subroutine UVMAT, load subroutine VDLOAD
triad
- 使用triad算法 解算星敏感器下的导弹姿态-Use triad algorithm solver star sensor under the Missile Attitude
daodan
- 仿真了弹道导弹在大气层上方的自由飞行段和重新进入大气层的再入段的飞行过程，可以作为初学者的参考。-Simulation of ballistic missiles above the atmosphere again free flight segment and re-entry into the atmosphere during the flight load segments can be used as reference.