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越肩发射是一种新型的攻击方式,要使导弹能够快速攻击尾后目标,且为了避免程序控制导弹转弯这种方式不够灵活,载机无法根据目标机动快速调整导弹转向的缺点,提出了一种由本机发射电磁波束引导导弹转弯并对目标实施攻击的方法。首先分析了波束引导过程,在载机发射的波束指引下,计算出导弹的飞行弹道,并分析引导过程中导弹过载的变化,采用搜索算法模拟出了导弹的全向截获区;然后设计出导弹攻击方案,并计算出此方案下机上波束发射装置的转动规律。最后通过仿真分析,证明了该方法的实用性和有效性。
Shoulder launch is a new type of attack, to make the missile quickly attack the tail after the target, and in order to avoid the program control of the missile turning this way is not flexible enough, the carrier can not be based on the target maneuver to quickly adjust the shortcomings of missile steering, proposed a A method of turning a missile and launching a target attack by launching electromagnetic beams from this unit. Firstly, the beam guidance process is analyzed. Under the guidance of beam launched by the carrier, the missile trajectory is calculated and the change of the missile overloading during the guidance process is analyzed. The search algorithm is used to simulate the omnidirectional interception area of the missile. Attack scheme, and calculate the program under the aircraft beam launcher rotation rules. Finally, the simulation analysis shows that the method is practical and effective.