{"title":"导航误差下目标跟踪的施密特-卡尔曼滤波设计","authors":"Chun Yang, Erik Blasch, P. Douville","doi":"10.1109/AERO.2010.5446689","DOIUrl":null,"url":null,"abstract":"In most target tracking formulations, the tracking sensor location is typically assumed perfectly known. Without accounting for navigation errors of the sensor platform, regular Kalman filters tend to be optimistic (i.e., the covariance matrix far below the actual mean squared errors). In this paper, the Schmidt-Kalman filter (SKF) is formulated for target tracking with navigation errors. The SKF does not estimate the navigation errors explicitly but rather takes into account (i.e., considers) the navigation error covariance provided by an on-board navigation unit in the tracking filter formulation. Including the navigation errors leads to the so-called “consider covariance.” By exploring the structural navigation errors, the SKF is not only more consistent but also produces smaller mean squared errors than regular Kalman filters. Monte Carlo simulation results are presented in the paper to demonstrate the operation and performance of the SKF for target tracking in the presence of navigation errors.1,2","PeriodicalId":378029,"journal":{"name":"2010 IEEE Aerospace Conference","volume":"39 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2010-03-06","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"14","resultStr":"{\"title\":\"Design of Schmidt-Kalman filter for target tracking with navigation errors\",\"authors\":\"Chun Yang, Erik Blasch, P. Douville\",\"doi\":\"10.1109/AERO.2010.5446689\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"In most target tracking formulations, the tracking sensor location is typically assumed perfectly known. Without accounting for navigation errors of the sensor platform, regular Kalman filters tend to be optimistic (i.e., the covariance matrix far below the actual mean squared errors). In this paper, the Schmidt-Kalman filter (SKF) is formulated for target tracking with navigation errors. The SKF does not estimate the navigation errors explicitly but rather takes into account (i.e., considers) the navigation error covariance provided by an on-board navigation unit in the tracking filter formulation. Including the navigation errors leads to the so-called “consider covariance.” By exploring the structural navigation errors, the SKF is not only more consistent but also produces smaller mean squared errors than regular Kalman filters. Monte Carlo simulation results are presented in the paper to demonstrate the operation and performance of the SKF for target tracking in the presence of navigation errors.1,2\",\"PeriodicalId\":378029,\"journal\":{\"name\":\"2010 IEEE Aerospace Conference\",\"volume\":\"39 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2010-03-06\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"14\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2010 IEEE Aerospace Conference\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/AERO.2010.5446689\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2010 IEEE Aerospace Conference","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/AERO.2010.5446689","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Design of Schmidt-Kalman filter for target tracking with navigation errors
In most target tracking formulations, the tracking sensor location is typically assumed perfectly known. Without accounting for navigation errors of the sensor platform, regular Kalman filters tend to be optimistic (i.e., the covariance matrix far below the actual mean squared errors). In this paper, the Schmidt-Kalman filter (SKF) is formulated for target tracking with navigation errors. The SKF does not estimate the navigation errors explicitly but rather takes into account (i.e., considers) the navigation error covariance provided by an on-board navigation unit in the tracking filter formulation. Including the navigation errors leads to the so-called “consider covariance.” By exploring the structural navigation errors, the SKF is not only more consistent but also produces smaller mean squared errors than regular Kalman filters. Monte Carlo simulation results are presented in the paper to demonstrate the operation and performance of the SKF for target tracking in the presence of navigation errors.1,2