弹射发射反坦克导弹发射动力学分析

通过理论分析和测试，建立了包括导弹，发射筒和发射支架的弹射反坦克导弹发射动力学分析随机模型，设计了分析计算程序，用于分析计算发射过程红外光轴振动，导弹的初始扰动和无控飞行段的散布，预估导弹射入可控域的概率和发射支架的稳定性。该模型和计算程序适用于多种发射方式和制导方式的反坦克导弹发射动力学分析。

LAUNCHING DYNAMICS ANALYSIS OF AN EJECTOR LAUNCHED ANTI-TANK MISSILE

On the basis of theoretical analysis and testing, a launching dynamics analysis with an accompanying random model that includes the missile, the launching tube, and the launching support of an anti-tank missile weapon system is established. A corresponding computer program can be used to perform the analytical computation of the vibration of the infrared light axis during the launching process, the initial disturbance of the missile, and the random distribution of the missile during the uncontrolled flight stage. As a result of the above mentional analysis, probability of the missile to be launched into the controlable zone and the stability of the support can be estimated. The model and computer program provided in this paper are applicable to the launching dynamics analysis of similar anti-tank missile systems with different launching methods and modes of control.