{"title":"飞行器在空气动力作用下的非线性控制","authors":"D. Pucci, T. Hamel, P. Morin, C. Samson","doi":"10.1109/CDC.2013.6760648","DOIUrl":null,"url":null,"abstract":"The paper contributes towards the development of a unified control approach for longitudinal aircraft dynamics. It states conditions that allow to adapt the control strategies developed for orientation-independent external forces to the orientation-dependent case. The control strategy presented here is a step to the automatic monitoring of the flight transitions between hovering and cruising for convertible aerial vehicles.","PeriodicalId":415568,"journal":{"name":"52nd IEEE Conference on Decision and Control","volume":"117 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2013-12-10","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"16","resultStr":"{\"title\":\"Nonlinear control of aerial vehicles subjected to aerodynamic forces\",\"authors\":\"D. Pucci, T. Hamel, P. Morin, C. Samson\",\"doi\":\"10.1109/CDC.2013.6760648\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The paper contributes towards the development of a unified control approach for longitudinal aircraft dynamics. It states conditions that allow to adapt the control strategies developed for orientation-independent external forces to the orientation-dependent case. The control strategy presented here is a step to the automatic monitoring of the flight transitions between hovering and cruising for convertible aerial vehicles.\",\"PeriodicalId\":415568,\"journal\":{\"name\":\"52nd IEEE Conference on Decision and Control\",\"volume\":\"117 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2013-12-10\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"16\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"52nd IEEE Conference on Decision and Control\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/CDC.2013.6760648\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"52nd IEEE Conference on Decision and Control","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/CDC.2013.6760648","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Nonlinear control of aerial vehicles subjected to aerodynamic forces
The paper contributes towards the development of a unified control approach for longitudinal aircraft dynamics. It states conditions that allow to adapt the control strategies developed for orientation-independent external forces to the orientation-dependent case. The control strategy presented here is a step to the automatic monitoring of the flight transitions between hovering and cruising for convertible aerial vehicles.
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