Improved SINS/CNS Integrated Navigation System with Fault Detection Based on Statistical Distance

Guangle Gao, Shesheng Gao, Xu Peng, Jiahao Zhang, Bingbing Gao, Zhaohui Gao
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Abstract

Celestial navigation system (CNS) is a completely autonomous navigation technology with strong anti-interference ability and high navigation accuracy, which has a great application prospect. Aim at defect of traditional integrated navigation system using attitude angle measurement celestial navigation system and strapdown inertial navigation system (SINS), which can only correct of strapdown inertial navigation system’s gyro drift. This paper proposes an improved integrated navigation system that add double-star positioning celestial navigation to traditional SINS/CNS integrated navigation system, meanwhile, introduces the fault detection technology based on statistical distance to solve the problem that inaccuracy of measurement information leads to the integrated navigation system’s performance degradation. By analyzing the simulation results, the improved navigation system can inhibit divergence of system and obtain high accurate and stable navigation information.
基于统计距离故障检测的改进SINS/CNS组合导航系统
天体导航系统(CNS)是一种抗干扰能力强、导航精度高的完全自主导航技术,具有很大的应用前景。针对传统组合导航系统采用姿态角测量天文导航系统和捷联惯导系统(SINS)的缺陷,只能对捷联惯导系统的陀螺漂移进行校正。本文提出了一种改进的组合导航系统,在传统SINS/CNS组合导航系统基础上增加双星定位天体导航,同时引入基于统计距离的故障检测技术,解决了测量信息不准确导致组合导航系统性能下降的问题。仿真结果表明,改进后的导航系统能够抑制系统发散,获得高精度、稳定的导航信息。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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