摘要
具有快速机动发射能力的弹道导弹是现代远程作战武器的重要标志,提出了无依托快速发射的定位、定向方案,设计了基于空中在线诸元计算的摄动制导方法,该方法具有计算量小、制导方法误差小的特点,可满足陆基机动弹道导弹或潜射弹道导弹的快速发射的要求。
The ballistic missile with fast mobile launch capability is the important symbol of modern long-range weapon.In this paper,the positioning and orientation scheme of offhand fast launch is submitted,and the perturbation guidance method based on air online data computation is designed.The small computation load and guidance method error of the proposed method can meet the fast launch requirements for ground-based mobile ballistic missile and submarine-launched ballistic missile.
出处
《宇航学报》
EI
CAS
CSCD
北大核心
2010年第8期1915-1919,共5页
Journal of Astronautics
关键词
无依托发射
在线诸元计算
组合制导
摄动制导
Offhand launch
Online data computation
Integrated guidance
Perturbation guidance