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ProportionalNavigationGuidanceEmuator
- 用比例导引律仿真拦截器拦截来袭导弹的时间步长模拟算法,MT弹道数据,具体自己定-Proportional guidance law simulation interceptor missiles to intercept incoming time-step simulation algorithm, MT ballistic data, specific itself
Trajectory-Program
- 本程序为风干扰下弹道解算程序,包括matlab程序和simulink程序,非常实用-The procedures for the wind interference under ballistic solver, including the the matlab procedure and simulink program, very useful