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本文讨论一种控制规律,它能改进倾斜转弯控制导弹在形成和实施先进制导规律上存在的主要缺点。这种控制规律已经经过六自由度仿真验证,在发射包线内,其脱靶距离可限制在4～5英尺以内。与线性制导相比,缩短了飞行时间,减小了发射包线内边界,在其内发射边界内,它甚至以近乎常数的最太控制仍可击中目标。
This article discusses a control law that improves the major drawbacks of tilting turn control missiles in the formation and implementation of advanced guidance laws. This control law has been verified by six-degree-of-freedom simulation in the launch envelope, the off-target distance can be limited to 4 to 5 feet. Compared with linear guidance, the flight time is shortened, the inner boundary of the transmission envelope is reduced, and within its inner emission boundary, it can hit the target even with the most constant near-maximum control.