{"title":"基于扩展卡尔曼滤波的非线性TACAN轴承跟踪伺服系统设计","authors":"S. Welt","doi":"10.1109/CDC.1988.194406","DOIUrl":null,"url":null,"abstract":"An analytical and simulation study was used to develop a near-real-time optimum digital computer TACAN bearing tracking algorithm. An extended Kalman filter estimator was utilized to determine a tracking loop configuration and its expected performance. Examination of the filter covariance matrix and gains revealed that a few key elements of the covariance matrix were the significant contributors to the filter gains. This observation suggested that a set of time-switched constant gains multiplied by the partial derivatives of the observation with respect to the state would provide adequate performance with significant real-time processing reduction. Fortran computer simulations verified the concept. The algorithm was implemented on a microcomputer, and the system was successfully flight-tested.<<ETX>>","PeriodicalId":113534,"journal":{"name":"Proceedings of the 27th IEEE Conference on Decision and Control","volume":"112 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1988-12-07","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"Design of a nonlinear TACAN bearing tracking servo using the extended Kalman filter\",\"authors\":\"S. Welt\",\"doi\":\"10.1109/CDC.1988.194406\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"An analytical and simulation study was used to develop a near-real-time optimum digital computer TACAN bearing tracking algorithm. An extended Kalman filter estimator was utilized to determine a tracking loop configuration and its expected performance. Examination of the filter covariance matrix and gains revealed that a few key elements of the covariance matrix were the significant contributors to the filter gains. This observation suggested that a set of time-switched constant gains multiplied by the partial derivatives of the observation with respect to the state would provide adequate performance with significant real-time processing reduction. Fortran computer simulations verified the concept. The algorithm was implemented on a microcomputer, and the system was successfully flight-tested.<<ETX>>\",\"PeriodicalId\":113534,\"journal\":{\"name\":\"Proceedings of the 27th IEEE Conference on Decision and Control\",\"volume\":\"112 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1988-12-07\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Proceedings of the 27th IEEE Conference on Decision and Control\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/CDC.1988.194406\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceedings of the 27th IEEE Conference on Decision and Control","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/CDC.1988.194406","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Design of a nonlinear TACAN bearing tracking servo using the extended Kalman filter
An analytical and simulation study was used to develop a near-real-time optimum digital computer TACAN bearing tracking algorithm. An extended Kalman filter estimator was utilized to determine a tracking loop configuration and its expected performance. Examination of the filter covariance matrix and gains revealed that a few key elements of the covariance matrix were the significant contributors to the filter gains. This observation suggested that a set of time-switched constant gains multiplied by the partial derivatives of the observation with respect to the state would provide adequate performance with significant real-time processing reduction. Fortran computer simulations verified the concept. The algorithm was implemented on a microcomputer, and the system was successfully flight-tested.<>