The development environment for the MATLAB6.5 version of the program, prepared by the programs to be run in this environment. Due to the aerodynamic model of discrete, and adopted a number of empirical formula for calculation and experimental data, so the programming will be more complex, in order to make the program easier to read clear, in compiling a program with the following idea: taking into account the general structure of the program, where aerodynamic calculation system is divided into three modules: input module, pneumatic calculation modules and output modules. Taking into account the specificity of this system, in turn divided into initial data input module input module, module and interpolation of shape parameters of missiles database modules, and




File list:
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