A predictive research for the range of hood separation and landing locations considering multiple factors

The separation process of missile hood is influenced by many kinds of uncertain factors, along with limited trial number of target range and interplay between influencing factors, thus it is difficult to precisely determine separation process and hood landing locations. The aim of this study is to establish dynamic simulation model of hood separation and landing track based on Monte-Carlo method. From repeated digital simulation calculations considering many influential factors, statistics parameters of landing location are obtained. This study provides a technical support for facilities protection on launching site.