火箭时序参数判读方法分析与改进

摘要

Following analysis of the advantages and disadvantages of the current processing methods for the time sequence parameters of rocket launches, an optimized processing method is proposed to reduce mistaken and missed processing. Built on segmented processing and accumulated processing, the method uses different processing approaches based on the reliability of time sequence parameters of rocket launches through a correlation process. As a result, processing of the time sequence parameters of rocket launches is significantly improved. It is a valuable exploration into a new approach for processing of the time sequence parameters of rocket launches and it provides more dependable technical support for analysis of the state of rocket launches.%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.