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高密度集成微惯性导航自主完好性监测OA北大核心CSTPCD

Autonomous integrity monitoring of integrated micro-inertial navigation system

中文摘要英文摘要

针对多平台、小型化、集群化等未来微小型空天飞行器故障信息自主监测等技术需求,提出了一种高密度集成微惯性导航自主完好性监测算法.该算法依托最优估计理论,分析微惯性导航系统中可能出现的量测误差信息源,通过优选子集数目进行预检验甄选,利用牛顿恒等式优化工程计算方法,达到微惯性导航系统故障信息检测与排除的目的.与传统MHSS算法相比,该算法能够显著降低系统的计算复杂度,并可有效检测小差错和多差错故障观测量,具有较高的故障信息源检测识别概率,增强了高密度集成微惯性导航与制导系统鲁棒性和完备性.

Aiming at the problem of future multi-domain high-intensity operations,such as strong confrontation,multi-platform,miniaturization and clustering,a high-density integrated micro-inertial navigation autonomous integrity monitoring algorithm was proposed,which relys on the optimal estimation theory.It analyzes the information sources of measurement errors that may appear in the micro-inertial navigation system,performs pre-check selection by optimizing the number of subsets,and uses Newton's identity to optimize the engineering computational complexity to achieve the purpose of fault detection and elimination.Compared with the traditional MHSS algorithm,the computational complexity in micro-system could be greatly reduced,small-error and multi-error fault observations could be effectively detected simultaneously,which improves integrity and robustness of high-density integrated micro-inertial guidance and navigation systems.

孟凡琛;宋健民;邢朝洋;王巍

北京航天控制仪器研究所,北京 100094中国航天科技集团有限公司,北京 100048

高密度集成微惯性导航组合导航完好性监测鲁棒性

high density integrationmicro systemcombination navigationintegrity monitoringrobustness

《中国空间科学技术》 2024 (001)

34-43 / 10

国家自然科学基金基础科学中心项目(62388101),中国科协青年人才托举工程(2021QNRC001)

10.16708/j.cnki.1000-758X.2024.0004

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