Confidence interval solution for whole missile system based on approximate Bayesian limits method

The Bayes method can be used to evaluate the performance of missile guider and control system. It leads an easy way to obtain the anti-jamming probability and confidence interval of both guider and control systems respectively, however the confidence interval of the whole system is difficult to compute. The approximate Bayesian limit method was introduced to solve the problem of the confidence interval, and a formula of the approximate confidence interval was derived. Finally, the correctness of the approximate Bayesian limit method was validated through simulation.