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.
出处
《弹箭与制导学报》
CSCD
北大核心
2006年第4期30-33,共4页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
再人机动
制导
姿态控制
六自由度仿真
maneuvering reentry
guidance t attitude control
six-degree-of-freedom simulation
