摘要
结合近程战术地地导弹控制系统滚动回路的设计，讨论了整个设计过程中的设计思想和设计方法。针对导弹的弹体滚动运动参数在较大范围内变化的特点，将回路校正网络设计为变参数校正网络。设计中，使用ＩＥＡＳ语言编程对滚动回路单通道和控制回路三通道进行计算机仿真，经多次协调设计，结果令人满意。给出了部分仿真结果。
he Design idea and method for the roll loop of control system in some short-range taotieal surface-to-surface missile are discussed. The loop calibration network is designed as a variable parameter calibration network in the light of the property of the missile's body rollmovement parameters varied within a larger range. The computer simulation of single channel in roll loop and three channel in control loop is madeby using IEAS. languge programming la design. The results are satisfactory through many times of coordinated designs. The portion of the simulation results is given.
出处
《上海航天》
1995年第5期19-22,共4页
Aerospace Shanghai
