基于HLA的脉冲修正火箭弹仿真平台设计  

Design of Impulse Correction Rocket Simulation Platform Based on HLA

作　　者：胡杰[1] 黄长强[1] 刘安[1] 崔亮[2] 

机构地区：[1]空军工程大学工程学院,西安710038 [2]94857部队77分队,芜湖241007

出　　处：《系统仿真学报》2009年第5期1324-1328,共5页Journal of System Simulation

基　　金：空军工程大学优秀博士学位论文创新基金(BC08002)

摘　　要：基于HLA提供的框架和标准,对脉冲修正火箭弹的仿真方法进行了研究,介绍了联邦结构,提出了火箭弹的数学模型,给出了FOM/SOM设计和时间管理方法。根据仿真流程,采用MK Technologies公司的MK RTI,借助Visual C++6.0实现联邦仿真平台的设计。通过实例仿真可知,该平台可用于确定火箭弹战术技术指标,并可完成模拟作战训练任务。Based on the framework and standards provided by HLA （High Level Architecture）, simulation method of impulse correction rocket was studied. The federation structure was introduced and mathematical model of the rocket was brought forward. FOM （Federation Object Model）/SOM （Simulation Object Model） and time management of the federation were also designed. According to simulation flow, federation simulation platform was designed in MAK RTI and Visual C＋＋6.0. An example was simulated in the platform. Results show that the platform can be applied to design technique and tactic indexes of the rocket and battle-training mission can be simulated in the platform.

关 键 词：高层体系结构 联邦 脉冲修正 仿真平台 

分 类 号：TP391.9[自动化与计算机技术—计算机应用技术]