{"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}
引用次数: 1
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.<>