The interdiction effectiveness problem was described with probability integral method for the runway cut-blanked modes of intelligence, when entry angle error and open cabin position error exist. On the condition of open cabin position error determined, the allowable range of entry angle error was inversely calculated with interdiction probability. The calculated results indicate that the method men?tioned can manifest the intelligence missile interdiction efficiency to the runway and the range of entry angle error, which provides available basis for analyzing the intelligence missile attack assignment on tne way.
Key words
operational research /
intelligence missile /
blanking probability /
inverse calculation /
bullet block
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Footnotes
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