Модель процесса наведения авиационной противокорабельной ракеты в условиях перерыва поступления информации

In this article was developed a mathematical model of guidance process of an anti-ship missile (ASM), having a structure with two possible states which are defined by existence or absence of information about target. For creation of optimum guidance of ASM, it is necessary to go by the way of simplifications of initial differential equations system describing functioning of dynamic object, which allow decreasing its order. Further, to define the equations of the optimum linear filter and an optimum regulator than include them in initial system then include them in guidance law. The optimal filter work in two operation modes: the first is filtration regime when the information is available and the second is memory mode when the incoming information about target is interrupted.