直接力/气动力复合控制系统快速原型设计  

Rapid Prototype Design on Reaction-jet /Aerodynamic Compound Control System

作　　者：郭雯雯[1] 马慧敏[1,2] 龚铮[1] 

机构地区：[1]中国空空导弹研究院,河南洛阳471009 [2]航空制导武器航空科技重点实验室,河南洛阳471009

出　　处：《四川兵工学报》2013年第12期71-74,共4页Journal of Sichuan Ordnance

摘　　要：针对传统导弹飞控系统开发周期长、效率低的现状,设计了一种基于RT-LAB环境的直接力/气动力复合控制系统快速原型仿真系统;首先建立了直接力/气动力复合控制弹体动力学模型,在此基础上,利用快速原型开发平台,通过高速串口和数据采集板卡(422),实现仿真代码的实时生成,并与视景仿真系统结合,完成快速原型样机的实时仿真及同步视景演示;试验结果表明:系统具有良好的有效性和实时性。As for the disadvantages of long-term development cycle and low efficiency according to tradi-tional missile flight control system, a reaction-jet/aerodynamic control system is designed on rapid proto-type, which is based on RT-LAB. First, reaction-jet/aerodynamic control system model is constructed. By calling the RT-LAB, the real-time simulation is realized through high-speed serial board and data acquisi-tion card （422）. Combining the visual simulation, the synchronous visual demo of the real-time simulation is carried out. The results show that this system has favorable effectiveness and real-time capability.

关 键 词：RT—LAB 快速原型 控制系统 实时仿真 视景仿真 

分 类 号：TP391.9[自动化与计算机技术—计算机应用技术]