Research on Missile Six Degrees of Freedom Model in RF Guidance Simulation System

Shi Chuan, He Rongmao, W. Lihua
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Abstract

In the RF guidance simulation system, the software simulation of the missile flight model is one of the key technologies to be solved. This paper introduces the theoretical basis of missile flight modeling, and deeply studies the missile six degree of freedom mathematical model and its simulation algorithm. The missile flight trajectory simulation was carried out with Visual C++.Then the simulation results were used to analyze the accuracy and real-time of the two simulation algorithms, which provided a reference for the next modeling and simulation work.
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导弹射频制导仿真系统中的六自由度模型研究
在射频制导仿真系统中,导弹飞行模型的软件仿真是需要解决的关键技术之一。介绍了导弹飞行建模的理论基础,深入研究了导弹六自由度数学模型及其仿真算法。利用visualc++对导弹飞行轨迹进行仿真。然后利用仿真结果分析了两种仿真算法的精度和实时性,为下一步的建模和仿真工作提供参考。
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