{"title":"Maximum Principle Solutions for Time-Optimal Half-Loop Maneuvers of a High Alpha Fighter Aircraft","authors":"H. Stalford, Eric A. Hoffman","doi":"10.23919/ACC.1989.4790600","DOIUrl":null,"url":null,"abstract":"In this paper we present a maximum principle solution of the half-loop maneuver obtained using an analytical model for a high alpha fighter aircraft and compare it with that obtained previously using a simple nonlinear feedback control law derived from singular perturbation analysis.","PeriodicalId":383719,"journal":{"name":"1989 American Control Conference","volume":"1 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1989-06-21","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"6","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"1989 American Control Conference","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.23919/ACC.1989.4790600","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 6
Abstract
In this paper we present a maximum principle solution of the half-loop maneuver obtained using an analytical model for a high alpha fighter aircraft and compare it with that obtained previously using a simple nonlinear feedback control law derived from singular perturbation analysis.
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