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为了减少火箭时序参数判读过程中的误判和漏判,通过分析比较现有的火箭时序参数判读方法的优缺点,提出了结合判读的新方法。该方法以分段判读和累积判读为基础,先采用相关判定的方法判断火箭飞行中实时获取的时间基准参数的可靠性,再根据可靠性的不同选取不同的判读方法,从而有效地减少误判和漏判现象的发生。为改进火箭时序参数判读方法探索了新的途径,为分析火箭飞行状态提供了更可靠的支持。
In order to reduce the misjudgment and omission of rocket timing parameter interpretation, by analyzing and comparing the advantages and disadvantages of existing rocket timing parameter interpretation methods, a new method combining interpretation is proposed. Based on the staged interpretation and cumulative interpretation, this method firstly uses the method of correlation judgment to judge the reliability of the time reference parameters acquired in real time in rocket flight, and then selects different interpretation methods according to the different reliability so as to effectively reduce the misjudgment And missed the occurrence of the phenomenon. In order to improve the rocket timing parameter interpretation method to explore new ways to provide more reliable support for the analysis of rocket flight status.