摘要
参考坐标系是导弹飞行力学研究的基础。本文针对某型制导航弹的特点建立了斜置坐标系 ,并且给出了斜置坐标系之间以及斜置坐标系与常规坐标系之间的转化关系。
Reference coordinate system is the basis of research on the dynamics of flight for missiles. Considering the characteristics of a guided bomb, the paper establishes a series of sideling coordinate systems. The transformation relation between sideling coordinate systems and the transformation relation between the sideling coordinate system and groovy coordinate system are given. The simulation results of research on the equations of motion of guided bomb established in sideling coordinate system show the advantages of the sideling coordinate system.
出处
《兵工学报》
EI
CAS
CSCD
北大核心
2002年第2期201-204,共4页
Acta Armamentarii
关键词
制导航弹
飞行力学
参考坐标系
航空炸弹
guided bomb, dynamics of flight, reference coordinate system
