再入机动弹头控制系统六自由度仿真  

Six-degree-of-freedom Simulation of Control System for Reentry Maneuver Warhead

作　　者：王龙[1] 刘新学[1] 

机构地区：[1]第二炮兵工程学院,西安710025

出　　处：《弹箭与制导学报》2006年第4期30-33,共4页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：使用制导和姿态控制系统一体化的设计思想,建立了弹头六自由度仿真的数学模型,实现了连续系统与离散系统的混合仿真,使用Visual C++语言开发了仿真软件,经过仿真试验,证明该模型与传统三自由度模型相比更精确、更符合实际,验证了仿真系统的可信性。Using integrated design idea of guidance and attitude control system, the paper establishes a six-degree-of-freedom simulation system of a warhead and accomplishes mixed simulation of continuous system and discrete system. The simulation software is programmed by use of Visual C＋＋. After many simulation experimentations, this model is proved more accurate and more practical than three-degree-of-freedom simulation model. The creditability of the system is validated.

关 键 词：再人机动 制导 姿态控制 六自由度仿真 

分 类 号：TJ765[兵器科学与技术—武器系统与运用工程]