Title:
proportional-guidance-law
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Description: Proportional guidance law is introduced，and trajectory equation of intercepting missile based
on proportional guidance law is deduced．A kind of orbit equation of target in sine mobility is given，and
the missile intercepting the target is simulated with Matlab．The influence of missile speed，target speed
and guidance mode on the trajectory is analyzed．The relationship between trajectory curvature and normal
over-loading is researched．
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基于Matlab的比例导引导弹仿真分析.pdf
proportional guidance law.pdf
