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通过导弹垂直发射阶段的分析,可以确定垂直发射方式应用于近程导弹的可能性.本报告研究了助推加速度、转弯开始时间、俯仰速率指令限值和推力矢量控制偏转指令限值等导弹参数对在最小的高度上作急转弯要求的影响.文章最后将采用推力矢量控制的导弹的性能与只采用气动力控制的类似导弹作比较,结果表明,对于具有推力矢量控制的近程导弹来说,垂直发射是一种很有前途和很有吸引力的发射方式.
Through the analysis of the vertical launching phase of the missile, the possibility of applying the vertical launch mode to short-range missiles can be determined.This report studies missile parameters such as boost acceleration, turn start time, pitch rate command limit, and thrust vector control deflection command limits On the minimum height of the sharp turns for the requirements of the impact.Finally, the article will use thrust vector control of the missile performance and only the use of aerodynamic control of similar missiles compared the results show that for the thrust vector control with short-range missiles Vertical launch is a promising and attractive launch mode.