{"title":"Optimal Rocket Maneuvers in Space","authors":"M. Pachter, G. Chatterji, M. Tahk","doi":"10.1109/ACC.1989.4173543","DOIUrl":null,"url":null,"abstract":"The problem is addressed of optimally steering a vehicle in space, controlled by thrust vectoring, to affect a demanded change in heading and achieve maximal terminal speed. The optimal solution is explicitly derived and it is presented in a readily implementable form.","PeriodicalId":383719,"journal":{"name":"1989 American Control Conference","volume":"176 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1989-06-21","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"1989 American Control Conference","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ACC.1989.4173543","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
Abstract
The problem is addressed of optimally steering a vehicle in space, controlled by thrust vectoring, to affect a demanded change in heading and achieve maximal terminal speed. The optimal solution is explicitly derived and it is presented in a readily implementable form.
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