| 导弹制导控制系统半实物仿真系统的设计与实现 |
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| 引用本文： | 耿东平,王正平,郝磊.导弹制导控制系统半实物仿真系统的设计与实现[J].飞行力学,2008,26(5). |
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| 作者姓名： | 耿东平 王正平 郝磊 |
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| 作者单位： | 1. 西北工业大学,航空学院,陕西,西安,710072
2. 第二炮兵装备研究院第五装备研究所,北京,100085 |
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| 摘 要： | 为了更有效地对导弹制导与控制技术进行研究,设计了一种以仿真技术和弹上计算机相结合的测试系统。通过仿真计算机输出相应的加速度脉冲给弹上计算机,弹上计算机输出反馈信号给仿真计算机,从而实现测试系统的闭环工作。该测试系统能同时考察弹上多种硬件设备及飞行控制程序的工作状态,对优化制导与控制方法有较大的帮助。
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| 关 键 词： | 导弹 制导 半实物仿真 |
Design and Implementation of Hardware-in-the-Loop Simulation System for Missile Control and Guidance System |
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| GENG Dong-ping,WANG Zheng-ping,HAO Lei.Design and Implementation of Hardware-in-the-Loop Simulation System for Missile Control and Guidance System[J].Flight Dynamics,2008,26(5). |
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| Authors: | GENG Dong-ping WANG Zheng-ping HAO Lei |
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| Institution: | 1.College of Aeronautics;Northwestern Polytechnical University;Xi;an 710072;China;2.The Fifth Research Institute;The Second Artillery Equipment Academy;Beijing 100085;China |
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| Abstract: | A test system based simulation method and computer of the missile is designed for efficient research on missile's control and guidance method.The simulation computer sends acceleration impulse to computer of the missile and the computer of the missile sends feedback signal to the simulation computer,which realizes the system work in the closed loop.This system can optimize missile's control and guidance method,because it can test many kinds of missile units and program of missile control. |
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| Keywords: | missile control and guidance hardware-in-the-loop simulation |
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