Title:
Aerodynamicmissileprogram
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Description: This procedure for the development environment MATLAB6.5 version, the proceedings shall be made to run in this environment. Due to the discreteness of the aerodynamic model, and used a lot of experience in engineering calculation formula and experimental data, it would be more complicated programming, in order to facilitate a clear reading procedure, the procedure used in the preparation of the following ideas:
Procedures, taking into account the general structure of computing systems here will be divided into three pneumatic modules: input module, pneumatic calculation module, as well as the results of the output module. Taking into account the specificity of the system, will enter the module is divided into the initial data input module, the missile shape parameter interpolation module and database module, and the use of M file format aerodynamic calculation module uses the structure subsystem, and the preparation of Simulink module the results of output module is used in the for
File list (Check if you may need any files):
MATLAB(Simulink)程序
....................\Aerodynamic.mdl
....................\Calculate.m
....................\Configulation_data.m
....................\Draw_Figure.m
....................\Flight_data.m
....................\Interpolation_data.m
....................\Start_file.m
程序说明.doc
