逃逸追逐问题仿真工具包

该程序包涵盖了二维空间导弹拦击目标问题的各种仿真模拟程序，其中导弹和目标模型均采用低保真度模型，即假设导弹和目标均为质点运动模型，程序包中讨论了各种工况因素对导弹导引律设计的影响和注意事项。求解器采用二阶龙格库塔方法，以保证求解精度。制导拦截仿真包括开环和闭环两种，其中开环仿真采用真实信息生成导引指令；闭环仿真采用滤波器提供的状态估计生成导引指令。

5th IBM MATLAB
slprj
C10L1.M
C10L2.M
C11L1.M
C12L1.M
C12L2.M
C12L3.M
C12L4.M
C13L1.M
C13L2.M
C14L1.M
C14L2.M
C14L3.M
C14L4.M
C15L1.M
C15L2.M
C16L1.M
C16L2.M
C16L3.M
C17L1.M
C17L2.M
C18L1.M
C19L1.M
C19L2.M
C1L1.m
C1L2.m
C20L1.M
C20L2.M
C20L3.M
C20L4.M
C20L5.M
C21L1.M
C21L2.M
C21L3.M
C21L4.M
C22L1.M
C22L2.M
C23L1.M
C23L2.M
C23L3.M
C23L4.M
C24L1.M
C24L2.M
C24L3.M
C25L1.M
C25L2.M
C26L1.M
C26L2.M
C26L3.M
C27L1.M
C27L2.M
C27L3.M
C27L4.M
C28L1.M
C28L2.M
C28L3.M
C28L4.M
C28L5.M
C28L6.M
C29L1.M
C29L2.M
C2L1.m
C2L2.m
C30L1.M
C30L3.M
C30L5.M
C30L6.M
C3L1.m
C4L1.m
C4L2.m
C4L3.m
C4L4.m
C4L5.m
C4L6.m
C5L1.m
C5L2.m
C5L3.m
C6L1.m
C6L2.m
C7L1.m
C7L2.m
C7L3.m
C7L4.m
C8L1.m
C8L2.m
C9L1.M
C9L2.M
C9L3.M
datfil.txt
DISTANCE.m
DISTANCE3D.m
GAUSS.m
GAUSSC7.m
GENERATEGAINS.m
INITIAL.m
KEPLER1.m
LAMBERT.m
LAMBERT3D.m
OLAMBERT.m
PREDICT.m
PREDICT1.m
PREDICTB.m
PREDICTG.m
PREDICTP.m
pvMPPT1_sfun.mexw32
UNIFORM.m