{"title":"飞机自适应控制系统的混合仿真","authors":"P. W. Halbert","doi":"10.1145/1463822.1463867","DOIUrl":null,"url":null,"abstract":"The general concept of adaptive control has become well known, and the objectives and various types of adaptive systems have been classified. In particular, for adaptive control of a high performance aircraft, it is desired to alter the feedback control parameters in the basic linear control system to correct for unknown, unanticipated, or unaccounted-for changes in the aircraft's operating characteristics, inputs, or criterion of performance.","PeriodicalId":432708,"journal":{"name":"AFIPS '63 (Fall)","volume":"39 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1899-12-30","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"Hybrid simulation of an aircraft adaptive control system\",\"authors\":\"P. W. Halbert\",\"doi\":\"10.1145/1463822.1463867\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The general concept of adaptive control has become well known, and the objectives and various types of adaptive systems have been classified. In particular, for adaptive control of a high performance aircraft, it is desired to alter the feedback control parameters in the basic linear control system to correct for unknown, unanticipated, or unaccounted-for changes in the aircraft's operating characteristics, inputs, or criterion of performance.\",\"PeriodicalId\":432708,\"journal\":{\"name\":\"AFIPS '63 (Fall)\",\"volume\":\"39 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1899-12-30\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"AFIPS '63 (Fall)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1145/1463822.1463867\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"AFIPS '63 (Fall)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1145/1463822.1463867","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Hybrid simulation of an aircraft adaptive control system
The general concept of adaptive control has become well known, and the objectives and various types of adaptive systems have been classified. In particular, for adaptive control of a high performance aircraft, it is desired to alter the feedback control parameters in the basic linear control system to correct for unknown, unanticipated, or unaccounted-for changes in the aircraft's operating characteristics, inputs, or criterion of performance.