{"title":"基于动态反演的非线性飞行控制器设计","authors":"Y. Baba, L. Takano, M. Sano","doi":"10.1109/SICE.1995.526734","DOIUrl":null,"url":null,"abstract":"This paper deals with a synthesis for a nonlinear flight controller using a nonlinear state feedback. This method is called a dynamic inversion theory and is widely used to design a nonlinear flight controller. We show how to choose the control gains for the controller designed by a dynamic inversion theory when inversion is not exact due to the actuator lags.","PeriodicalId":344374,"journal":{"name":"SICE '95. Proceedings of the 34th SICE Annual Conference. International Session Papers","volume":"29 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1995-07-26","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":"{\"title\":\"Design of a nonlinear flight controller based on dynamic inversion\",\"authors\":\"Y. Baba, L. Takano, M. Sano\",\"doi\":\"10.1109/SICE.1995.526734\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper deals with a synthesis for a nonlinear flight controller using a nonlinear state feedback. This method is called a dynamic inversion theory and is widely used to design a nonlinear flight controller. We show how to choose the control gains for the controller designed by a dynamic inversion theory when inversion is not exact due to the actuator lags.\",\"PeriodicalId\":344374,\"journal\":{\"name\":\"SICE '95. Proceedings of the 34th SICE Annual Conference. International Session Papers\",\"volume\":\"29 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1995-07-26\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"2\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"SICE '95. Proceedings of the 34th SICE Annual Conference. International Session Papers\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/SICE.1995.526734\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"SICE '95. Proceedings of the 34th SICE Annual Conference. International Session Papers","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/SICE.1995.526734","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Design of a nonlinear flight controller based on dynamic inversion
This paper deals with a synthesis for a nonlinear flight controller using a nonlinear state feedback. This method is called a dynamic inversion theory and is widely used to design a nonlinear flight controller. We show how to choose the control gains for the controller designed by a dynamic inversion theory when inversion is not exact due to the actuator lags.