An Engineering Method of the Missile Impact Accuracy Evaluation
Minghai Wang · Flight Dynamics · 2004
This paper discusses the complete mathematic model of an engineering missile impact evaluation by Bayes method and presents a new thought and method of determining the missile impact error prior information by combining and making the most of the missile flight test prior guidance apparatus error demarcation information and the flight test error separate information.It also addresses the corresponding mathematic model and finally presents a missile evaluation example. This method not only ensures the prior information veracity and reliability, but also ensures the missile impact accuracy and evaluation accuracy, and reliability by Bayes method.