{"title":"基于最优性的弹道整形制导设计","authors":"Qinghong Wang, Ching-Fang Lin, C. D'souza","doi":"10.1109/AEROCS.1993.721055","DOIUrl":null,"url":null,"abstract":"A design and implementation scheme for the trajectory shaping guidance is discussed in this paper. The guidance law is assumed to be in some feedback form with unknown gains. The gains are then parameterized and obtained by solving a finite-dimensional parameter optimization problem. The advantage of this approach is that the control law would be in a feedback form while maintaining optimality. Furthermore, the design parameters are exactly the guidance parameters for implementing a guidance law.","PeriodicalId":170527,"journal":{"name":"Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,","volume":"12 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1993-05-25","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Optimality-Based Trajectory Shaping Guidance Design\",\"authors\":\"Qinghong Wang, Ching-Fang Lin, C. D'souza\",\"doi\":\"10.1109/AEROCS.1993.721055\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"A design and implementation scheme for the trajectory shaping guidance is discussed in this paper. The guidance law is assumed to be in some feedback form with unknown gains. The gains are then parameterized and obtained by solving a finite-dimensional parameter optimization problem. The advantage of this approach is that the control law would be in a feedback form while maintaining optimality. Furthermore, the design parameters are exactly the guidance parameters for implementing a guidance law.\",\"PeriodicalId\":170527,\"journal\":{\"name\":\"Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,\",\"volume\":\"12 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1993-05-25\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/AEROCS.1993.721055\",\"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. The First IEEE Regional Conference on Aerospace Control Systems,","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/AEROCS.1993.721055","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
A design and implementation scheme for the trajectory shaping guidance is discussed in this paper. The guidance law is assumed to be in some feedback form with unknown gains. The gains are then parameterized and obtained by solving a finite-dimensional parameter optimization problem. The advantage of this approach is that the control law would be in a feedback form while maintaining optimality. Furthermore, the design parameters are exactly the guidance parameters for implementing a guidance law.
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