摘要
为找到一条理想的EKV末段逆轨拦截弹道,基于零控拦截的理想情形进行了相应假设,设计了零控拦截弹道确定过程,完成了EKV末段拦截弹道建模。根据公开的OBV飞行试验资料综合分析了EKV拦截时机和空域,从而为仿真环境的具体构建提供了有益参考,仿真结果与逆轨拦截的实际情形是相符的。
In order to find out a perfect contra-interception trajectory of EKV, the presumption was proposed based on zero effort interception, the process of finding an interception trajectory based on zero effort interception was designed, and the model of terminal phase interception trajectory was accomplished. Interception opportunity and airspace of EKV were considered synthetically by exoteric data of the OBV flight-testing to offer a beneficial reference for practical environment building of simulation, and the simulation result is consistent with the factual case.
出处
《飞行力学》
CSCD
北大核心
2010年第2期75-77,81,共4页
Flight Dynamics
关键词
自由段
零控拦截
脱靶量
拦截时机
拦截空域
vacuum flight phase
zero effort interception
miss distance
interception opportunity
airspace of interception
