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Research on Missile-borne Computer Closed Loop Simulation System Based on Six-degree-of-freedom Model
Pages: 65-69
Year: Issue:  5
Journal: AEROSPACE CONTROL

Keyword:  六自由度模型弹载计算机闭环仿真弹道导弹;
Abstract: 提出了基于导弹六自由度模型,将弹载计算机置于导弹闭环仿真回路,从而构成对弹载计算机进行考核的半实物仿真方法.通过建立导弹六自由度模型,在分析弹载计算机信号接口和软件特点的基础上,对弹载计算机闭环仿真系统的硬件组成和工作原理进行了论述.通过采用高性能的仿真计算机、实时积分算法、智能化接口设备和基于PCI总线的数据通讯方式几个方面,保证了半实物仿真的实时性.
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