Description: The Matlab program calculates the longitudinal three degrees of freedom of a reentry module that requires high speed passage through the atmosphere. Only basic parameters such as initial velocity, reentry height and reentry angle are entered. There are more detailed instructions in the program. The atmospheric model uses the real 1976 American Standard atmosphere model, which contains the Matlab program for calculating the standard atmospheric model. Only the input height and height interval can be used to find the detailed parameter values.
To Search:
File list (Check if you may need any files):
三自由度仿真
三自由度仿真\自由度仿真
三自由度仿真\自由度仿真\Standard_Density.mat
三自由度仿真\自由度仿真\all_six_time.m
三自由度仿真\自由度仿真\func_six_time.m
三自由度仿真\自由度仿真\runge_kuttal.m
三自由度仿真\自由度仿真\程序说明.txt
三自由度仿真\计算标准大气参数
三自由度仿真\计算标准大气参数\Standard_Atmosphere.mat
三自由度仿真\计算标准大气参数\atmo.m
三自由度仿真\计算标准大气参数\atmo_compo.m
三自由度仿真\计算标准大气参数\atmo_p.m
三自由度仿真\计算标准大气参数\atmo_temp.m
三自由度仿真\计算标准大气参数\f_n.m
三自由度仿真\计算标准大气参数\int_tau.m
三自由度仿真\计算标准大气参数\tester.m
Download