摘要
The blockage effectiveness problem for the runway cut-blanked modes of intelligence missile is described using probability integral method,when entry angle error and open cabin position error exist. On the condition of determined open cabin position error,the allowable range of entry angle error is inversely calculated with interdiction probability. The calculated results indicate that the method mentioned can estimate 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 the way.
The blockage effectiveness problem for the runway cut-blanked modes of intelligence missile is described using probability integral method, when entry angle error and open cabin position error exist. On the condition of determined open cabin position error, the allowable range of entry angle error is inversely calculated with interdiction probability. The calculated results indicate that the method mentioned can estimate 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 the way.
