{"title":"Optimal path and tracking control of an autonomous VTOL aircraft","authors":"A. Ailon","doi":"10.1109/MED.2006.328771","DOIUrl":null,"url":null,"abstract":"This study presents a simple algorithm for motion-planning and design tools for tracking in a vertical take-off and landing (VTOL) aircraft. The proposed motion-planning procedure is based on the solution of a linear algebraic equation. The resulting schemes are useful for flight control of an autonomous VTOL aircraft in case the objective is to drive the system from a given state to a prescribed target and when a reference path should be followed. In particular the proposed controller ensures the accomplishment of a required control task while in addition, a selected quadratic index of performance is minimized. The solution to the suboptimal control problem is simple since a functional which measures the controller performance, reduces to a quadratic form and hence, the extremum is associated with a minimum point of a function of several variables","PeriodicalId":347035,"journal":{"name":"2006 14th Mediterranean Conference on Control and Automation","volume":null,"pages":null},"PeriodicalIF":0.0000,"publicationDate":"2006-06-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"3","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2006 14th Mediterranean Conference on Control and Automation","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/MED.2006.328771","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 3
Abstract
This study presents a simple algorithm for motion-planning and design tools for tracking in a vertical take-off and landing (VTOL) aircraft. The proposed motion-planning procedure is based on the solution of a linear algebraic equation. The resulting schemes are useful for flight control of an autonomous VTOL aircraft in case the objective is to drive the system from a given state to a prescribed target and when a reference path should be followed. In particular the proposed controller ensures the accomplishment of a required control task while in addition, a selected quadratic index of performance is minimized. The solution to the suboptimal control problem is simple since a functional which measures the controller performance, reduces to a quadratic form and hence, the extremum is associated with a minimum point of a function of several variables
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