{"title":"LDV approach to circular trajectory tracking of the underactuated hovercraft model","authors":"F. Ariaei, E. Jonckheere","doi":"10.1109/ACC.2006.1657329","DOIUrl":null,"url":null,"abstract":"This paper shows that circular trajectory tracking of an underactuated hovercraft vehicle can be achieved by linear dynamically varying (LDV) techniques. LDV control is a technique for directing a controlled trajectory to be asymptotically synchronized with a preselected trajectory. A linearized tracking error model is obtained as a linear system parameterized by the nominal nonlinear dynamics. The nontrivial part of the LDV theory is to prove existence of a sufficiently well behaved solution to the partial differential Riccati equation. This in turn provides an exact solution to a Lyapunov inequality, showing that the underactuated hovercraft can be stabilized around the circular trajectory","PeriodicalId":265903,"journal":{"name":"2006 American Control Conference","volume":"30 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2006-06-14","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"9","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2006 American Control Conference","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ACC.2006.1657329","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 9
Abstract
This paper shows that circular trajectory tracking of an underactuated hovercraft vehicle can be achieved by linear dynamically varying (LDV) techniques. LDV control is a technique for directing a controlled trajectory to be asymptotically synchronized with a preselected trajectory. A linearized tracking error model is obtained as a linear system parameterized by the nominal nonlinear dynamics. The nontrivial part of the LDV theory is to prove existence of a sufficiently well behaved solution to the partial differential Riccati equation. This in turn provides an exact solution to a Lyapunov inequality, showing that the underactuated hovercraft can be stabilized around the circular trajectory