摘要
基于空间目标快速拦截问题,设计并优化了共轨、共面两种空间轨道快速拦截模型,其中共面快速拦截设计了高轨目标拦截和低轨目标拦截两种模型。在每一种快速拦截模型中均详细分析了拦截时机、机动冲量、拦截轨道等参数。采用HLA体系架构并通过VC平台编码实现分布式仿真验证系统,与STK/Connect模块与STK/Astrogator模块实现互联,充分解决了验证系统的快速整合问题,最后仿真并验证了各种快速拦截模型的正确性。
Based on the problem of space target quick interception, common rail and coplanar model of space target interception were designed and optimized, and coplanar model included high-rail and low-orbit target interception models. In every model, intercept time, maneuver impulse, and interception orbit were all analyzed in details. The distributed verification system was implemented through VC platform with the use of HLA architecture, and interconnected with STK/Connect module and STK/Astrogator module, which could solve the quick integration issue. At last, every quick interception model accuracy was verified through simulation.
出处
《系统仿真学报》
CAS
CSCD
北大核心
2013年第10期2390-2396,共7页
Journal of System Simulation
