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本文研究非旋转式导弹控制系统的模态解耦能力。证明了具有俯仰、偏航和滚动三个控制通道的控制系统可以实现俯仰、偏航两种运动模态对滚动运动模态的完全解耦。给出了模态解耦控制系统的设计方法。对一种导弹控制系统进行了验证性设计,做了数字仿真。
This paper studies the modal decoupling ability of a non-rotating missile control system. It is proved that the control system with three control channels of pitch, yaw and roll can realize the complete decoupling of the rolling motion modes by both pitch and yaw motion modes. The design method of modal decoupling control system is given. A verification design of a missile control system was made and digital simulation was done.