Airplane Vulnerability Of Built Model Method And Dmeca Of Software Development

Suvivability is mainly made up of two parts, namely susceptibility and vulnerability. Identifying the critiacal components is the basis for vulnerability assessment. This thesis has studied the method of identifying the critiacal components of aircraft and a sorftware of critiacal component identfication has been developed for vulnerability analysers . It also analyses several problems involved in computing the aircraft kill probability and the kill methods of missle's destroying the target. Though studying one of the methods of establishing aircraft models for vulnerability assessment, we can get the geometric model, structure model ,critiacal component model .Those models can be used for computer simulation. This thesis has also proposed an algorithm calculating the presented areas, overlapping areas of critical components for vulnerabe areas ejaculation hi each standard aspect.