Research on integrated navigation of strap-down inertial navigation system and star sensor

Z. Minghui, Wang Qiuying, Guo Zheng
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引用次数: 3

Abstract

Sail for a long time in the sea, and the inertial navigation system error accumulating with time affect navigation accuracy seriously, meanwhile the star sensor can output the high precision information. So inertial navigation / Star integrated navigation technology is applied to solve this problem. Through the strap-down inertial navigation system and the star sensor, the position information of the ship is calculated during the navigation process, and the difference of the position information is taken as the observation quantity. Then, the Kalman filter is used to fuse the data information, so as to estimate effectively the integrated navigation system error terms. The purpose is to modify the navigation information of the inertial navigation system. Through the system simulation, it can be seen that this combination navigation method can effectively suppress the divergence of the inertial navigation system error and improve the navigation accuracy when navigating the ship.
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捷联惯导系统与星敏感器组合导航研究
在海上长期航行,惯性导航系统误差随时间累积严重影响导航精度,而星敏感器可以输出高精度信息。因此采用惯性导航/星组合导航技术来解决这一问题。通过捷联惯导系统和星敏感器,在导航过程中计算船舶的位置信息,并将位置信息的差值作为观测量。然后,利用卡尔曼滤波对数据信息进行融合,从而有效地估计组合导航系统的误差项。目的是修改惯导系统的导航信息。通过系统仿真可以看出,该组合导航方法可以有效抑制惯导系统误差发散,提高船舶导航精度。
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