为了控制导弹飞向目标,必须确保制导设备与导弹外形和控制系统之间的兼容性,必须使系统的主要部件参数最佳化,以获得可能的最佳性能。为此,进行整个导弹系统的模拟和仿真是必不可少的。这里,所谓模拟和仿真两者之间的些微差别是:仿真时有硬件参加,因而是实时的模拟。模拟的基本原理很早之前就有了,开始是用微分分析方法。把伺服机构之间的大量联系 In order to control the missiles toward the target, the compatibility of the guidance equipment with the missile profile and the control system must be ensured and the parameters of the system's main components must be optimized for the best possible performance. For this reason, the simulation and simulation of the entire missile system are indispensable. Here, the slight difference between the so-called simulation and the simulation is that there is hardware participation in the simulation and therefore real-time simulation. The basic principle of simulation has long ago, the beginning is the use of differential analysis. A lot of links between the servo