节点文献
捷联惯导系统大方位失准角下的非线性对准
SINS Nonlinear Alignment with Large Azimuth Misalignment Angles
【摘要】 采用欧拉角描述平台坐标系与导航坐标系间的失准角,推导了适用于捷联惯导系统的非线性误差方程,证明了该方法仅适用于方位误差角为大角度,而水平误差角为小量的情况。数学仿真表明:在方位误差角为大角度情况下,采用所推导的误差方程和非线性滤波技术能获得更高的估计精度。
【Abstract】 Luler angles are adopted to describe the misalignment of platform to navi-gation frame. It was pointed out that the derived error medels are only valid when the head-ing uncertainty is large and the level misalignment angles are small. The simulation resultsshow that, under large azimuth misalignment, good alignment accuracy can be obtained us-ing the derived nonlinear error models and nanlinear filtering techniques.
【关键词】 惯性导航;
非线性滤波;
初始对准;
【Key words】 Inertial navigation; Error model; Initial alignment; Nonlinear filtering;
【Key words】 Inertial navigation; Error model; Initial alignment; Nonlinear filtering;
- 【文献出处】 航天控制 ,Aerospace Control , 编辑部邮箱 ,2003年04期
- 【分类号】V249.3
- 【被引频次】40
- 【下载频次】534