本发明涉及一种自推进导弹的导向系统。在采用这种导向系统时,导弹在两个位置上被导向,这两个位置在纵向上彼此相隔一段距离。人们熟悉的自推进导弹的导向系统一方面可由导向装置(可以是一个管子或者是一种滑轨系统)组成,另一方面也可由导弹本身的导向环(可以是导环,导轮或者其它类似的元件)组成。在采用人们熟悉 The present invention relates to a self-propelled missile guidance system. In employing such a guidance system, the missile is guided in two locations that are longitudinally separated from each other by a distance. The guided self-propelled missile guidance system can be composed of a guide device (which can be a pipe or a sliding rail system) on the one hand and a guide ring of the missile itself (which can be a guide ring, a guide wheel or the like) Of components). Familiar with people