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一体化导弹六自由度全量数学仿真系统的设计与实现
引用本文:焦勇,强金辉,周喻虹.一体化导弹六自由度全量数学仿真系统的设计与实现[J].弹箭与制导学报,2007,27(3):103-105.
作者姓名:焦勇  强金辉  周喻虹
作者单位:中国兵器工业第203研究所,西安,710065
摘    要:在建立导弹大规模复杂仿真系统时往往需要实现功能完善、人机界面友好的一体化仿真环境,使之集仿真试验、数据处理和可视化显示于一体.文中给出了一种一体化导弹六自由度运动全量数学仿真系统的设计及实现方式,该软件基于面向对象方法分析、设计和实现,具有仿真条件配置、仿真运行控制、仿真结果可视化显示和数据即时处理、输出等主要功能.在该仿真模型的基础上,扩展或者继承这些基础类模块,可以对各种导弹或飞行器的复杂运动模型进行建模和仿真.

关 键 词:导弹仿真  飞行仿真  一体化仿真
收稿时间:2006-02-13
修稿时间:2006-02-132006-12-05

Design and Implement of Integrated 6 DOF Missile Simulation System
JIAO Yong,QIANG Jin-hui,ZHOU Yu-hong.Design and Implement of Integrated 6 DOF Missile Simulation System[J].Journal of Projectiles Rockets Missiles and Guidance,2007,27(3):103-105.
Authors:JIAO Yong  QIANG Jin-hui  ZHOU Yu-hong
Abstract:The integrated simulation system with excellent function and friendly UI is needed in development of large scale and complicated missile simulation system, which integrates simulation, visual display and real time data processing in result. This paper introduced a method of designing and implementing this kind integrated missile 6 DOF simulation system. Analysis, design and implement of this software is based on object-oriented method, and its main functions includes simulation condition configuration, dynamic control, visual display and real time data processing and output of data of simulation result. Base on this simulation model, we can construct various models of missile or aircraft.
Keywords:missile simulation  flight simulation  integrated simulation
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