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利用非线性系统干扰可解耦的条件及干扰解耦控制方法，可以对一个导弹拦截运动学系统进行解耦，从而得到一种不受目标切向机动干扰影响的导引规律。
Using the conditions of decoupling non-linear system disturbances and the decoupling control method of disturbance, a missile interception kinematics system can be decoupled to obtain a guidance law that is not affected by the target tangential maneuvering disturbance.