地空导弹装备指挥系统中的脆性传递过程分析  

ANALYSIS OF BRITTLENESS TRANSFER PROCESS IN EQUIPMENT COMMAND SYSTEM OF GROUND TO AIR MISSILE

作　　者：汪禹喆[1,2] 周林[1] 王毅[1] 张海林[1] WANG Yuzhe ZHOU Lin WANG Yi ZHANG Hailin(Missile Institute, Air Force Engineering University, Xi＇an 710051 Air Troops of 95607, Chengdu 61000 Missile Institute, Air Force Engineering University, Xi＇an 710051)

机构地区：[1]空军工程大学防空反导学院,西安710051 [2]95607部队,成都610000

出　　处：《系统科学与数学》2016年第11期2029-2040,共12页Journal of Systems Science and Mathematical Sciences

基　　金：部委级项目支持(2011KJ-0971Z);国家宇航动力学重点实验室对外基金项目(2012ADL-DW0301)资助课题

摘　　要：为客观描述地空导弹装备指挥系统(equipment command system,ECS)中的脆性传递过程,在ECS脆性特性的基础上,分步骤对ECS中的脆性传递过程进行了研究和讨论.首先.根据ECS个体间异常状态的互扰机制.提出了基于基本风险事件驱动的个体间基本脆性传递模式.之后,根据基本脆性传递模式和ECS中4类基本职能关系,提出了不同层级个体间基于职能关系的脆性传递方式.通过对地空导弹装备指挥实例的计算,得到了脆性传递过程中不同层级个体间的基本脆性数据和层级间的脆性传递数据,并且通过对数据的分析得出结论:脆性在ECS内的传递过程不仅满足脆性触发的基本机制,也符合实际指挥视角下对ECS风险及异常状态变化的一般性认识.In order to make objective description of brittleness transfer process in equipment command system （ECS） of Ground to Air Missile, this paper studies and discusses the brittleness transfer processes of ECS in steps depending on its brittle features. Sections 2 and 3 proposes the basic mode of risk-driven brittleness transfer processes based on abnormal state of interacting mechanism in ECS units. Then on the base of the previous section, Section 4 brings up the brittleness conduction pat- terns of ECS units according to the basic brittleness transfer mode under 4 functional relationships in ECS. By testing and analyzing the example of ECS, the following part gets brittleness data of ECS units in different levels during the brittleness transfer process. And the performance of the calculation demonstrates that the brittleness transfer process meets not only the basic brittleness trigger mechanism, but also the awareness of the risk and abnormal state which stays in the actual command view of ECS.

关 键 词：地空导弹 装备指挥 脆性 脆性传递模式 脆性传递 风险 

分 类 号：TJ762.13[兵器科学与技术—武器系统与运用工程]