摘要
针对机动弹头弹道导弹飞行的特点,应用六自由度一体化建模理论建立了较为精确的数学模型,并对其进行了仿真,给出了部分仿真结果。结果表明,所建立的六自由度运动模型能够充分表征其飞行特点,可在此基础上进一步进行系统分析、质量评估等工作。
Considering flying characteristic of the ballistic missile maneucvering reentry vehicle, applies the integrated modeling theory of six degree and simulates. It is can be infered by consequence that the model represent the characteristic of missile flying sufficiently, system analysis, quality evluation and some other work can be gone along next.
出处
《制导与引信》
2007年第2期13-15,41,共4页
Guidance & Fuze
关键词
机动弹头
导弹
仿真
maneuvering reentry vehicle
missile
simulation
