In this paper aimed at the application problem of certain aviation bomb for a certain fighter, a coincidental calculation method of bomb ballistic coefficient is proposed. 针对某型战机上挂载使用某型航空炸弹的问题,提出了一种炸弹弹道系数(BETA)的符合计算方法。
Different models of ballistic coefficient are studied and the properties of these models are comparied by simulation. 文章对弹道系数(BETA)的不同模型进行了研究并利用仿真结果对模型进行了适用性比较。
This paper analyzes the dominating factors that influence damping ballistic coefficient of one dimension trajectory correction fuze, brings forward that it is a precondition of optimize and simulation for damping ballistic coefficient to work out the time of calculating ballistic trajectory and the distance of maximum range correction. 首先分析了影响一维弹道修正引信阻尼弹道系数(BETA)选取的主要因素,提出了弹道解算时间和最大射程修正量的确定是计算最佳阻尼弹道系数(BETA)的的前提。
Optimize and Simulation for damping ballistic coefficient of one dimension trajectory correction fuze 一维弹道修正引信阻尼弹道系数(BETA)的优化与仿真
The ballistic coefficient formula of the energetic mini corner reflector is derived. 推导出动力型微型角反射器的弹道系数(BETA)计算公式;