{"title":"基于牛顿力学的新型重力干扰补偿惯性导航方法","authors":"Kaixin Luo;Ruihang Yu;Meiping Wu;Juliang Cao;Yulong Huang","doi":"10.1109/TIM.2024.3485437","DOIUrl":null,"url":null,"abstract":"With the continuous improvement of the accuracy of inertial devices and systems, the effects of gravity disturbance on autonomous inertial navigation system (INS) calculations cannot be overlooked. The traditional gravity disturbance compensation method directly introduces it into the INS calculation link, but the errors of gravity disturbance will lead to irreversible INS calculation errors, ultimately rendering the traditional compensation method ineffective. In this article, a new gravity disturbance compensation method for INS is proposed based on Newtonian mechanics. The INS calculation errors caused by horizontal gravity disturbance are directly corrected in the navigation system in a direct manner, which avoids coupling attitude calculation errors. The physical quantity of direct compensation is derived, and the influences of different compensation periods on the algorithm are tested. The effectiveness of the proposed method is validated using various sources of gravity disturbance. Both simulation and experimental results demonstrate that our method can effectively mitigate the influence of gravity disturbances on high-precision INSs.","PeriodicalId":13341,"journal":{"name":"IEEE Transactions on Instrumentation and Measurement","volume":null,"pages":null},"PeriodicalIF":5.6000,"publicationDate":"2024-10-23","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"A Novel Gravity Disturbance Compensation Inertial Navigation Method Based on Newtonian Mechanics\",\"authors\":\"Kaixin Luo;Ruihang Yu;Meiping Wu;Juliang Cao;Yulong Huang\",\"doi\":\"10.1109/TIM.2024.3485437\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"With the continuous improvement of the accuracy of inertial devices and systems, the effects of gravity disturbance on autonomous inertial navigation system (INS) calculations cannot be overlooked. The traditional gravity disturbance compensation method directly introduces it into the INS calculation link, but the errors of gravity disturbance will lead to irreversible INS calculation errors, ultimately rendering the traditional compensation method ineffective. In this article, a new gravity disturbance compensation method for INS is proposed based on Newtonian mechanics. The INS calculation errors caused by horizontal gravity disturbance are directly corrected in the navigation system in a direct manner, which avoids coupling attitude calculation errors. The physical quantity of direct compensation is derived, and the influences of different compensation periods on the algorithm are tested. The effectiveness of the proposed method is validated using various sources of gravity disturbance. Both simulation and experimental results demonstrate that our method can effectively mitigate the influence of gravity disturbances on high-precision INSs.\",\"PeriodicalId\":13341,\"journal\":{\"name\":\"IEEE Transactions on Instrumentation and Measurement\",\"volume\":null,\"pages\":null},\"PeriodicalIF\":5.6000,\"publicationDate\":\"2024-10-23\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"IEEE Transactions on Instrumentation and Measurement\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://ieeexplore.ieee.org/document/10731838/\",\"RegionNum\":2,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"ENGINEERING, ELECTRICAL & ELECTRONIC\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"IEEE Transactions on Instrumentation and Measurement","FirstCategoryId":"5","ListUrlMain":"https://ieeexplore.ieee.org/document/10731838/","RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, ELECTRICAL & ELECTRONIC","Score":null,"Total":0}
引用次数: 0
摘要
随着惯性设备和系统精度的不断提高,重力干扰对自主惯性导航系统(INS)计算的影响不容忽视。传统的重力扰动补偿方法直接将其引入 INS 计算环节,但重力扰动的误差会导致不可逆的 INS 计算误差,最终导致传统补偿方法失效。本文基于牛顿力学提出了一种新的 INS 重力扰动补偿方法。以直接方式在导航系统中直接修正由水平重力扰动引起的 INS 计算误差,避免了耦合姿态计算误差。推导了直接补偿的物理量,并测试了不同补偿周期对算法的影响。利用各种重力干扰源验证了所提方法的有效性。模拟和实验结果表明,我们的方法可以有效减轻重力干扰对高精度 INS 的影响。
A Novel Gravity Disturbance Compensation Inertial Navigation Method Based on Newtonian Mechanics
With the continuous improvement of the accuracy of inertial devices and systems, the effects of gravity disturbance on autonomous inertial navigation system (INS) calculations cannot be overlooked. The traditional gravity disturbance compensation method directly introduces it into the INS calculation link, but the errors of gravity disturbance will lead to irreversible INS calculation errors, ultimately rendering the traditional compensation method ineffective. In this article, a new gravity disturbance compensation method for INS is proposed based on Newtonian mechanics. The INS calculation errors caused by horizontal gravity disturbance are directly corrected in the navigation system in a direct manner, which avoids coupling attitude calculation errors. The physical quantity of direct compensation is derived, and the influences of different compensation periods on the algorithm are tested. The effectiveness of the proposed method is validated using various sources of gravity disturbance. Both simulation and experimental results demonstrate that our method can effectively mitigate the influence of gravity disturbances on high-precision INSs.
期刊介绍:
Papers are sought that address innovative solutions to the development and use of electrical and electronic instruments and equipment to measure, monitor and/or record physical phenomena for the purpose of advancing measurement science, methods, functionality and applications. The scope of these papers may encompass: (1) theory, methodology, and practice of measurement; (2) design, development and evaluation of instrumentation and measurement systems and components used in generating, acquiring, conditioning and processing signals; (3) analysis, representation, display, and preservation of the information obtained from a set of measurements; and (4) scientific and technical support to establishment and maintenance of technical standards in the field of Instrumentation and Measurement.