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实施舰载多管火箭武器系统发射姿态控制的目的 ,是提高火箭发射的精度。火箭发射过程中 ,载体存在 2种形式的振动 :随波振动和燃气流造成的冲击振动。因此系统的发射精度同时与船体的运动及发射系统的动力学结构特征等两方面因素密切相关。该文通过研究船体在火箭发射时的姿态及各姿态下火箭武器的发射特性 ,对发射时船体姿态求优 ,获得了对系统发射姿态实施控制的有效途径
The purpose of implementing the launch attitude control of the ship-borne multi-barrel rocket weapon system is to improve the accuracy of rocket launching. During rocket launching, there are two forms of vibration of the carrier: shock and vibration due to wave vibration and gas flow. Therefore, the launching accuracy of the system is closely related to both the movement of the hull and the dynamic structural characteristics of the launching system. In this paper, the attitude of the hull at launch is optimized by studying the attitude of the hull at launch time and the launching characteristics of the rocket weapon at each attitude, and an effective way to control the launching attitude of the system is obtained