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论述了一类空空导弹飞行控制系统的计算机辅助设计技术。设计特点是将根轨迹法与参数空间法两者相结合,利用MATLAB语言的图形用户界面设计工具开发了飞行控制系统的计算机辅助设计软件包,该软件充分利用了图形用户界面(Graphic User Interface,简称GUI)的优点,开发的界面友好,操作简单,并给出设计实例。
Discusses a kind of computer aided design technology of air-to-air missile flight control system. The design feature is the combination of root locus method and parametric space method. The computer aided design software package of flight control system is developed by using graphical user interface design tool of MATLAB language. This software makes full use of the graphical user interface Referred to as GUI) the advantages of friendly interface development, simple operation, and gives the design examples.