摘要
在惯性制导中,制导工具误差和基准误差是造成飞行器误差的主要原因,而卫星制导又易受外界环境的干扰,利用星敏感器的测量值,既可以修正工具误差和制导基准误差,又不受外界干扰的影响,因此星光制导在制导技术中得到广泛应用。通过研究初始对准修正方法,分析不同条件对修正效率的影响,提出初始对准方案使用的应用背景。
Guidance instrument error and reference error may cause error aircrafts in SINS. GPS guidance tends to be disturbed. Celestial navigation is widely used for its correction in guidance instru- ment error and reference error through measured value from star sensor and its anti-disturbance feature. The influence of correction efficiency in deferent situations has been analyzed and the application environment of initial alignment correction is proposed.
出处
《现代防御技术》
北大核心
2009年第6期41-43,共3页
Modern Defence Technology
关键词
星光制导
初始对准
修正效率
stellar guidance （ celestial navigation）
initial alignment
correction efficiency
